Capitolo 9 DEFORMAZIONI DELLE TRAVI F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.1 SOLUTION M K = 0 : − M0 + M = 0 M = M0 d2y = M = M0 dx dy EI = M 0 x + C1 dx EI dy x = L, dx = 0 : 0 = M 0 L + C1 EIy = [ x = L, y = 0] (a) 0= C1 = − M 0 L 1 M 0 x 2 + C1x + C2 2 1 M 0 L2 − M 0 L2 + C2 2 Elastic curve: C2 = 1 M 0 L2 2 y = M0 2 ( x − 2 Lx + L2 ) 2EI y = (b) y at x = 0 : (c) dy at x = 0 : dx yA = M0 ( L − 0) 2 2EI M0 ( L − x) 2 2EI yA = M 0 L2 ↑ 2 EI θA = w0 L EI dy M M M L = − 0 ( L − x) = − 0 ( L − 0) = − 0 dx EI EI EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.2 SOLUTION ΣM J = 0: − M − P( L − x) = 0 M = − P ( L − x) EI d2y = − P( L − x) = − PL + Px dx 2 EI dy 1 = − PLx + Px 2 + C1 dx 2 dy x = 0, dx = 0 : 0 = −0 + 0 + C1 C1 = 0 1 1 EIy = − PLx 2 + Px3 + C1x + C2 2 6 [ x = 0, y = 0] : (a) 0 = −0 + 0 + 0 + C2 C2 = 0 y =− Elastic curve. Px 2 (3L − x) 6 EI dy Px =− (2 L − x) dx 2 EI (b) y at x = L. (c) dy at x = L. dx yB = − dy dx =− B PL2 PL3 (3L − L) = − 6EI 3EI PL PL2 (2 L − L) = − 2EI 2EI yB = θB = PL3 ↓ 3EI PL2 2EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.3 SOLUTION ΣM J = 0: (wx) x +M =0 2 1 M = − wx 2 2 d2y 1 = M = − wx 2 2 dx 2 1 dy EI = − wx3 + C1 6 dx EI dy 1 3 1 3 x = L, dx = 0 : 0 = − 6 wL + C1 C1 = 6 wL EI dy 1 1 = − wx3 + wL3 dx 6 6 EIy = − 1 1 wx 4 + wL3 x + C2 24 6 [ x = L, y = 0] 0 = − 1 1 wL4 + wL4 + C2 = 0 24 6 1 3 1 C2 = − wL4 = − wL4 24 24 6 (a) Elastic curve. (b) y at x = 0. (c) dy at x = 0. dx y =− yA = − dy dx = A 3wL4 wL4 =− 24EI 8EI wL3 6EI w ( x 4 − 4 L3 x + 3L4 ) 24EI yA = θA = wL4 ↓ 8EI wL3 6 EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.4 SOLUTION Fy = 0: 1 wL = 0 2 1 RA = w0 L 2 RA = M A = 0: 2L wL ⋅ =0 3 2 1 = − w0 L2 3 − MA = MA ΣM J = 0: 1 1 w x2 x w0 L2 − w0 Lx + 0 ⋅ + M = 0 3 2 2L 3 1 1 w x3 M = − w0 L2 + w0 Lx − 0 3 2 6L EI 1 1 d2y w0 x3 2 = − + − w L w Lx 0 0 3 2 6L dx 2 1 1 dy w x4 = − w0 L2 x + w0 Lx 2 − 0 + C1 3 4 24L dx dy = 0, = 0 : 0 = −0 + 0 − 0 + C1 dx EI x C1 = 0 1 1 w x5 EIy = − w0 L2 x 2 + w0 Lx3 − 0 + C2 6 12 120L [ x = 0, y = 0] : 0 = −0 + 0 − 0 + 0 + C2 (a) Elastic curve: y =− C2 = 0 w0 1 3 2 1 1 5 Lx − Lx 4 + x EIL 6 12 120 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEM$ 9. (ContinuD) (b) y at x = L yB = − w0 L4 1 1 1 11 w0 L4 + − =− EI 6 12 120 120 EI yB = (c) dy at x = L dx dy dx =− B 11 w0 L4 ↓ 120 EI w0 L3 1 1 1 1 w0 L4 − + = − EI 3 4 24 8 EI θB = 1 w0 L3 8 EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.5 SOLUTION FBD ABC: Using ABC as a free body, ΣFy = 0: RA + 2wa − 2 wa = 0 3 4 4 RA = − wa = wa ↓ 3 3 2 ΣM A = 0: −M A + (2wa)(a) − wa (3a) = 0 3 MA = 0 Using AJ as a free body, FBD AJ: 4 x ΣM J = 0: M + wa ( x) − (wx) = 0 3 2 1 4 M = wx 2 − wax 2 3 d2y 1 4 = wx 2 − wax 2 2 3 dx dy 1 2 EI = wx3 − wax 2 + C1 dx 6 3 EI dy x = 0, dx = 0 : 0 = 0 − 0 + C1 ∴ C1 = 0 EIy = 1 2 wx 4 − wax3 + C2 24 9 [ x = 0, y = 0]: 0 = 0 − 0 + C2 ∴ C2 = 0 (a) Elastic curve over AB. (b) y at x = 2a. (c) dy at x = 2a. dx y = w (3x 4 − 16ax3 ) 72EI dy w 3 = ( x − 4ax 2 ) dx 6EI yB = − 10wa 4 9 EI 4wa3 dy = − 3EI dx B yB = θB = 10wa 4 ↓ 9 EI 4wa3 3EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.8 SOLUTION Reactions: 1 1 1 1 ΣM B = 0: − RA L + w0 L L − w0 L L = 0 2 3 4 6 1 RA = w0 L 8 Boundary conditions: [ x = 0, y = 0] [ x = L, y = 0] (0 ≤ x < L) For portion AB only, 1 1w x w0 Lx + 0 x ( x) + M = 0 8 2 L 3 1 1 w0 3 M = w0 Lx − x 8 6 L ΣM J = 0: − d2y 1 = w0 Lx − 8 dx 2 dy 1 EI w0 Lx 2 = dx 16 1 EIy = w0 Lx3 48 EI 1 w0 3 x 6 L 1 w0 4 x + C1 − 24 L 1 w0 5 − x + C1x + C2 120 L [ x = 0, y = 0] : 0 = 0 − 0 + 0 + C2 [ x = L, y = 0] : 0 = (a) 1 1 1 w0 L4 − w0 L4 + C1L C1 = − w0 L3 48 120 80 y = Elastic curve. C2 = 0 w0 1 2 3 1 5 1 4 Lx − x − L x 120 80 EIL 48 dy w 1 1 4 1 4 = 0 L2 x 2 − x − L 24 80 dx EIL 16 L . 2 (b) y at x = (c) dy at x = L. dx yL 2 = dy dx = B w0 EIL L5 L5 L5 15w0 L4 − − = − 3840EI 384 3840 160 w0 L4 L4 L4 2w L3 − − = + 0 EIL 16 24 80 240 EI yL 2 = θB = w0 L4 ↓ 256EI w0 L3 120 EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.11 SOLUTION Using entire beam as a free body, ΣM B = 0: M 0 − RA L = 0 RA = M0 L Using portion AJ , [ x = 0, y = 0] [ x = L, y = 0] ΣM J = 0: M 0 − M = M0 x+M =0 L M0 ( x − L) L d2y M = 0 ( x − L) 2 L dx dy M 1 = 0 x 2 − Lx + C1 EI dx L 2 EI EIy = [ x = 0, y = 0] 0 = 0 − 0 + 0 + C2 [ x = L, y = 0] 0= y = (a) M0 1 3 1 2 x − Lx + C1x + C2 2 L 6 M0 1 3 1 3 L − L + C1L + 0 2 L 6 M0 1 3 1 2 1 2 x − Lx + L x 2 3 EIL 6 To find location maximum deflection, set 1 2 1 xm − Lxm + L2 = 0 2 3 C2 = 0 1 M 0L 3 1 dy M 1 = 0 x 2 − Lx + L2 3 dx EIL 2 dy = 0. dx xm = L − 1 1 L2 − (4) L2 = 1 − 2 3 = 0.42265L ym = C1 = M 0 L2 1 1 1 3 2 (0.42265) − (0.42265) + (0.42265) EI 6 2 3 1 L 3 xm = 0.423L ym = 0.06415 M 0 L2 EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEM$ 9.11 (ContinuD Solving for M 0 , (b) Data: M0 = EIym 0.06415L2 E = 200 × 109 Pa, I = 178 × 106 mm 4 = 178 × 10−6 m 4 L = 3.5m M0 = ym = 1 mm = 10−3 m (200 × 109 )(178 × 10−6 )(10−3 ) = 45.3 × 103 N ⋅ m 2 (0.06415)(3.5) M 0 = 45.3 kN ⋅ m PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.14 SOLUTION Using ACB as a free body and noting that L = 3a, a M A = 0: RB L − (wa) = 0 2 [ x = 0, y = 0] [ x = L, y = 0] RB = ( wa) [ x = a, y = y] a 1 = wa 2L 6 dy dy x = a, dx = dx Fy = 0: RA + RB − wa = 0 0≤ x≤a MK = 0 : − M + RB ( L − x) = 0 x M − RA x + (wx) = 0 2 M = RB ( L − x) 1 2 wx 2 2 2 1 d y = RA x − wx 2 2 2 dx 1 dy 1 EI = RA x 2 − wx3 + C1 6 dx 2 1 1 EIy = RA x3 − wx 4 + C1 x + C2 6 24 EI [ x = 0, y = 0] 5 wa 6 a≤x≤L MJ = 0 : M = RA x − RA = 0 = 0 − 0 + 0 + C2 1 1 EIy = RA x3 − wx 4 + C1x 6 24 1 dy 1 2 3 = RA x − wx + C1 EI dx 2 6 C2 = 0 d y = RB ( L − x) dx 2 dy 1 EI = − RB ( L − x) 2 + C3 dx 2 1 EIy = RB ( L − x)3 + C3 x + C4 6 EI [ x = L, y = 0] 0 = 0 + C3 L + C4 C4 = − C3 L 1 RB ( L − x) 2 − C3 ( L − x) 6 1 dy EI = − RB ( L − x) 2 + C3 2 dx EIy = PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEMA 9.14 (Continua) dy dy 1 1 1 RAa 2 − wa3 + C1 = − RB (2a) 2 + C3 x = a, dx = dx 2 6 2 1 1 1 7 C3 = C1 + RAa 2 − wa3 + RB (2a) 2 = C1 + wa3 2 6 2 12 1 1 1 7 R Aa 3 − wa 4 + C1a = RB (2a)3 − C1 + wa3 (2a) 6 24 6 12 1 1 1 7 25 wa 4 + RB (2a)3 − wa 2 (2a) = − wa 4 3C1a = − RAa3 + 6 24 6 12 24 25 3 C1 = − wa 72 5 1 25 wax3 − wx 4 − wa3 x For 0 ≤ x ≤ a, EIy = 36 24 72 dy 5 1 25 EI wax 2 − wx3 − wa3 = dx 12 6 72 [ x = a, Data: y = y] w = 50 × 103 N/m, a = 2 m, E = 200 × 109 Pa I = 84.9 × 106 mm 4 = 84.9 × 10−6 m 4 , EI = 16.98 × 106 N ⋅ m 2 (a) Slope at x = 0. 16.98 × 106 dy dx dy dx (b) =0− 0− A 25 (50 × 103 )(2)3 72 = θ A = −8.18 × 10−3 θ A = 8.18 × 10−3 rad A Deflection at x = 2 m. 5 1 25 4 1 wa 4 − wa 4 − wa = − wa 4 36 24 72 4 1 16.98 × 106 yC = − (50 × 103 )(2)4 yC = − 11.78 × 10−3 m 4 EIyC = yC = 11.78 mm ↓ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.15 SOLUTION Reactions: RA = M 0 /L ↑, RB = M 0 /L ↓ M J = 0: 0 < x < a: M0 x+M =0 L M M= 0x L − [ x = 0, y = 0] [ x = L, y = 0] [ x = a, y = y] a < x < L: M K = 0: M0 x + M0 + M = 0 L M M = 0 ( x − L) L dy dy x = a, dx = dx − 0< x<a a< x< L d 2y M0 x = L dx 2 dy M 0 1 2 EI = x + C1 dx L 2 EI EIy = [ x = 0, M0 1 3 x + C1x + C2 L 6 y = 0] Eq. (2): d 2y M0 ( x − L) = L dx 2 dy M 0 1 2 EI = x − Lx + C3 dx L 2 EI (1) (2) 0 = 0 + 0 + C2 EIy = M0 1 3 1 2 x − Lx + C3 x + C4 2 L 6 (3) (4) C2 = 0 dy dy M0 1 2 M0 1 2 x = a, dx = dx Eqs. (1) and (3): L 2 a + C1 = L 2 a − La + C3 C3 = C1 + M 0a PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEMA 9.15 (Continua) [ x = a, y = y ] Eqs. (2) and (4): [ x = L, y = 0] Eq. (4): M0 L C1 = Elastic curve for 0 < x < a. M0 1 3 M0 1 3 1 2 a + C1a = a − La + ( C1 + M 0a)a + C4 L 6 L 6 2 1 C4 = − M 0a 2 2 1 1 3 1 3 2 L − L + (C1 + M 0a) L − M 0a = 0 6 2 2 M0 1 2 1 2 L + a − aL L 3 2 y= M0 1 3 1 2 1 2 x + L + a − aL x EIL 6 2 3 M0 1 3 1 2 1 M 2 1 a + L a + a3 − a 2 L = 0 a3 + L2a − La 2 EIL 6 3 2 EIL 3 3 Make x = a. yC = Data: E = 200 × 109 Pa, I = 34.4 × 106 mm 4 = 34.4 × 10−6 m 4 , M 0 = 60 × 103 N ⋅ m a = 1.2 m, L = 4.8 m yC = (60 × 103 ) (2)(1.2)3 / 3 + (4.8) 2 (1.2) / 3 − (4.8)(1.2)2 (200 × 109 )(34.4 × 10−6 )(4.8) = 6.28 × 10−3 m yC = 6.28 mm ↑ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.16 SOLUTION Consider portion ABC only. Apply symmetry about C. Reactions: RA = RE = P dy dy L dy = , x = , = 0 Boundary conditions: [ x = 0, y = 0], [ x = a, y = y], x = a, dx dx 2 dx 0< x<a a< x< L−a 2 EI d y = M = Px dx 2 EI dy 1 = Px 2 + C1 dx 2 EIy = d2y = M = Pa dx 2 dy EI = Pax + C3 dx 1 EIy = Pax 2 + C3 x + C4 2 EI (1) 1 3 Px + C1x + C2 6 (2) L dy 1 x = 2 , dx = 0 → C3 = − 2 PaL [ x = 0, y = 0] → C2 = 0 L dy dy x = 2 , dx = dx 1 2 1 Pa + C1 = Pa 2 − PaL 2 2 L x = 2 , y = y 1 3 1 2 1 1 1 Pa + Pa − PaL a = Pa3 − Pa 2 L + C4 6 2 2 2 2 C1 = C4 = (a) 1 2 1 Pa − PaL 2 2 1 3 Pa 6 Elastic curve for portion BD. y = 1 1 Pax 2 + C3 x + C4 EI 2 y = P EI 1 3 1 2 1 2 ax − 2 aLx + 6 a PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEMA 9.16 (Continua) For deflection at C, x= L . 2 yC = P EI set =− Data: 1 2 1 2 1 3 aL − aL + a 4 6 8 Pa 1 2 1 2 L − a EI 8 6 I = 23.9 × 106 mm 4 = 23.9 × 10−6 m 4 , E = 200 × 109 Pa P = 17.5 × 103 N, L = 2.5 m, a = 0.8 m (b) yC = − 2.52 0.82 (17.5 × 103 )(0.8) −3 − = −1.976 × 10 m 6 (200 × 109 )(23.9 × 106 ) 8 yC = 1.976 mm ↓ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.17 SOLUTION Boundary conditions are shown at right. [ x = 0, y = 0] [ x = L, V = 0] dy [ x = 0, = 0] dx [ x = L, M = 0] 2 dV x x = − w = − w0 1 − 4 + 3 dx L L 2 x 2 x3 + 2 + CV V = − w0 x − L L [ x = L, V = 0]: 0 = − w0 [ L − 2 L + L] + CV = 0 CV = 0 dM 2 x 2 x3 = V = − w0 x − + 2 dx L L x 2 2 x3 x4 M = − w0 − + 2 + CM 3L 4 L 2 2 1 1 [ x = L, M = 0]: 0 = − w0 L2 − L2 + L2 + CM 3 4 2 EI CM = 1 w0 L2 12 1 d2y 2 x3 1 x 4 1 2 = M = − w0 x 2 − + − L dx 3 L 4 L2 12 2 EI 1 1 x 4 1 x5 1 2 dy = − w0 x3 − + − L x + C1 6 L 20 L2 12 dx 6 [ x = 0, dy = 0] dx C1 = 0 1 1 x5 1 x6 1 2 2 EIy = − w0 x 4 − + − L x + C2 30 L 120 L2 24 24 [ x = 0, y = 0] C2 = 0 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEMA 9.17 (Continua) (a) Elastic curve. (b) Deflection at x = L. y=− yB = − w0 1 2 4 1 1 6 1 4 2 Lx − Lx5 + x − Lx 2 24 30 120 24 EIL w0 1 6 1 6 w0 L4 1 6 1 6 − + − = − L L L L 30 120 24 40 EI EIL2 24 yB = w0 L4 ↓ 40 EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.18 SOLUTION Boundary conditions at A and B are noted. w0 (4 Lx − 4 x 2 ) L2 w = −w = 20 (4 x 2 − 4Lx) L w 4 = V = 20 x3 − 2Lx 2 + C1 L 3 w= dV dx dM dx M = [ x = 0, M = 0] 0 = 0 + 0 + 0 + C2 [ x = L, M = 0] 0= EI w0 1 4 2 4 L − L + C1L + 0 3 L2 3 C1 = 1 w0 L 3 1 1 dy w 1 = 20 x5 − Lx 4 + L3 x 2 + C3 6 6 dx L 15 EIy = 1 1 3 3 w0 1 6 x − Lx5 + L x + C3 x + C4 2 30 18 L 90 [ x = 0, y = 0] 0 = 0 + 0 + 0 + 0 + C4 [ x = L, y = 0] 0= Elastic curve. C2 = 0 2 1 d2y w 1 = M = 20 x 4 − Lx3 + L3 x 2 3 3 dx L 3 EI (a) w0 1 4 2 3 x − Lx + C1x + C2 3 L2 3 C4 = 0 w0 1 6 1 6 1 6 L − L + L + C3L + 0 2 30 18 L 90 y = C3 = − 1 w0 L3 30 w0 1 6 1 1 3 3 1 5 x − Lx5 + Lx − L x 2 30 18 30 EIL 90 dy w0 1 5 1 4 1 3 2 1 5 = x − 6 Lx + 6 L x − 30 L dx EIL2 15 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEM 9.18 (ContinuD (b) (c) Set x = 0 in Slope at end A. Deflection at midpoint. Set x = dy . dx dy dx =− A 1 w0 L3 30 EI θA = 1 w0 L3 30 EI yC = 61 w0 L4 ↓ 5760 EI L in y. 2 6 5 3 w0 L4 1 1 1 1 1 1 1 1 yC = − + − EI 90 2 18 2 30 2 30 2 = w0 L4 1 1 1 1 61 w0 L4 − + − =− EI 5760 960 144 60 5760 EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.19 SOLUTION Reactions are statically indeterminate. Boundary conditions are shown above. Using free body AJ, ΣM J = 0: M 0 − RA x + M = 0 M = RA x − M 0 d2y = RA x − M 0 dx 2 1 dy EI = RA x 2 − M 0 x + C1 dx 2 EI dy 1 2 x = L, dx = 0 0 = 2 RA L − M 0 L + C1 C1 = M 0 L − EIy = 1 RA L2 2 1 1 RA x3 − M 0 x3 + C1x + C2 6 2 [ x = 0, y = 0] C2 = 0 [ x = L, y = 0] 0 = 1 1 1 RA L3 − M 0 L2 + M 0 L − RA L2 L + 0 6 2 2 RA = 3 M0 ↑ 2 L PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.20 SOLUTION Reactions are statically indeterminate. Boundary conditions are shown above. Using free body KB, L − x M K = 0: RB ( L − x) − w( L − x) −M =0 2 M = RB ( L − x) − 1 w( L − x) 2 2 d2y 1 = RB ( L − x) − w( L − x) 2 2 2 dx dy 1 1 = − RB ( L − x) 2 + w( L − x)3 + C1 EI dx 2 6 EI dy 1 1 3 2 x = 0, dx = 0 : 0 = − 2 RB L + 6 wL + C1 1 1 C1 = RB L2 − wL3 2 6 EI y = 1 1 RB ( L − x)3 − w( L − x) 4 + C1x + C2 6 24 1 RB L3 − 6 1 C2 = − RB L3 + 6 [ x = 0, y = 0]: 0 = 1 wL3 + C2 24 1 wL4 24 [ x = L, y = 0]: 0 = 0 − 0 + C1L + C2 1 1 1 1 RB L3 − wL4 − RB L3 + wL4 = 0 2 6 6 24 RB = 3 wL ↑ 8 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.21 SOLUTION Reactions are statically indeterminate. Boundary conditions are shown above. w0 ( L − x) L w = − w = − 0 ( L − x) L w 1 = V = − 0 Lx − x 2 + RA L 2 w= dV dx dM dx M =− EI w0 1 2 1 3 Lx − x + RA x L 2 6 d2y w 1 1 = − 0 Lx 2 − x3 + RA x 2 L 2 6 dx EI dy w 1 1 4 1 x + RA x 2 + C1 = − 0 Lx3 − dx L 6 24 2 EIy = − w0 1 1 5 1 Lx 4 − x + RA x3 + C1x + C2 L 24 120 6 [ x = 0, y = 0] dy x = L, dx = 0 0 = 0 + 0 + 0 + C2 − w0 1 4 1 4 1 L − L + RA L2 + C1 = 0 L 6 24 2 C1 = [ x = L, y = 0] − C2 = 0 1 1 w0 L3 − RA L2 8 2 w0 1 5 1 5 1 1 1 L − L + RA L3 + w0 L3 − RA L2 L = 0 L 24 120 6 2 8 1 1 1 1 1 2 − 6 RA = 8 − 24 + 120 w0 L 1 11 RA = w0 L 3 120 RA = 11 w0 L ↑ 40 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.22 L SOLUTION Reactions are statically indeterminate. Boundary conditions are shown above. Using free body JB, ΣM J = 0: −M + RB ( L − x) + + 1 2 w0 ( L − x) ( L − x) 2 3 1 w0 x 1 ( L − x) ( L − x ) = 0 2 L 3 w0 [2L( L − x) 2 + x( L − x) 2 ] 6L w = RB ( L − x) − 0 [2L3 − 4L2 x + 2Lx 2 + xL2 − 2 Lx 2 + x3 ] 6L w = RB ( L − x) − 0 ( x3 − 3L2 x + 2L3 ) 6L M = RB ( L − x) − d2y w = RB ( L − x) − 0 ( x3 − 3L2 x + 2L3 ) 2 6L dx 1 w 1 3 dy = RB Lx − x 2 − 0 x 4 − L2 x 2 + 2L3 x + C1 EI 2 6L 4 2 dx EI 1 w 1 1 1 EIy = RB Lx 2 − x3 − 0 x5 − L2 x3 + L3 x 2 + C1x + C2 6 6L 20 2 2 [ x = 0, y = 0] → C2 = 0 dy x = 0, dx = 0 → C1 = 0 1 1 1 w L4 1 [ x = L, y = 0] 0 = RB L3 − − 0 − + 1 2 6 6 20 2 1 1 11 RB = w0 L 3 6 20 RB = 11 w0 L ↑ 40 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.23 SOLUTION Reactions are statically indeterminate. Boundary conditions are shown at left. Using free body JB, MJ = 0 : [ x = 0, y = 0] [ x = L, y = 0] L − M + x dy = 0] [ x = 0, dx w0 2 ξ (ξ − x)d ξ + RB ( L − x) = 0 L2 w0 L 2 ξ (ξ − x)dξ − RB (L − x) L2 x M = L EI w0 1 4 1 3 ξ − xξ − RB ( L − x) 3 L2 4 x = 1 4 w0 1 4 1 3 L − Lx+ x − RB ( L − x) 2 3 12 L 4 d2y w 1 1 1 4 x − RB ( L − x) = 20 L4 − L3 x + 3 12 dx 2 L 4 EI dy w 1 1 1 5 1 x − RB Lx − x 2 + C1 = 20 L4 x − L3 x 2 + dx 6 60 2 L 4 EIy = dy x = 0, dx = 0 [ x = 0, y = 0] [ x = L, y = 0] Data: = w0 1 4 2 1 3 3 1 6 1 1 Lx + x − RB Lx 2 − x3 + C1x + C2 Lx − 18 360 2 6 L2 8 0 = 0 + 0 + C1 0 = 0 + 0 + 0 + C2 C1 = 0 C2 = 0 1 1 1 1 1 4 3 + − w0 L − − RB L = 0 8 18 360 2 6 13 1 13 w0 L4 − RB L3 = 0 RB = w0 L 180 3 60 L = 3m w0 = 15 kN/m 13 RB = (15)(3) = 9.75 kN 60 RB = 9.75 kN ↑ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.25 SOLUTION Reactions are statically indeterminate. ΣFy = 0: RA + RB = 0 ΣM A = 0: RA = − RB − M A − M 0 + RB L = 0 0 <x < M A = RB L − M 0 L 2 M = RB x + M A = −M 0 + RB L − RB x d2y = − M 0 + RB ( L − x) dx 2 1 dy EI = − M 0 x + RB Lx − x 2 + C1 dx 2 EI 1 1 1 EIy = − M 0 x 2 + RB Lx 2 − x3 + C1x + C2 2 6 2 L < x< L 2 M = RB ( L − x) d2y = RB ( L − x) dx 2 1 dy = RB Lx − x 2 + C3 EI dx 2 EI 1 1 EIy = RB Lx 2 − x3 + C3 x + C4 6 2 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEMA 9.25 (Continua) dy x = 0, dx = 0 0 + 0 + C1 = 0 C1 = 0 [ x = 0, y = 0] 0 + 0 + 0 + C2 = 0 C2 = 0 L dy dy x = 2 , dx = dx −M 0 L 1 1 1 1 + RB L2 − L2 = RB L2 − L2 + C3 2 6 6 2 2 C3 = − M 0L 2 L x = 2 , y = y 2 L 1 1 3 1 3 L 1 1 − M 0 + RB L3 − L = RB L3 − L + C3 + C4 2 2 48 48 2 8 8 1 1 C4 = − M 0 L2 − C3 L 8 2 1 1 1 = − + M 0 L2 = M 0 L2 8 8 4 [ x = L, y = 0] 1 M L 1 1 RB L3 − L3 + 0 L + M 0 L2 = 0 6 2 8 2 1 1 1 1 3 2 2 − 6 RB L = 2 − 8 M 0 L 1 3 M0 RB = 3 8 L RB = MA = 9 1 M0 − M0 = M0 8 8 M C − = −M 0 + 9 M0 7 = − M0 8 L 16 L 9 M0 L 9 M C + = RB L − = M0 = 2 8 L 2 16 9 M0 ↑ 8 L MA = 1 M0 8 M C− = − 7 M0 16 M C+ = 9 M0 16 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.26 SOLUTION Reactions are statically indeterminate. ΣFy = 0 : RA + RB − P = 0 RA = P − RB ΣM A = 0: − M A + M A = RB L − 0< x< 1 PL − RB L = 0 2 1 PL 2 1 L: 2 M = M A + RA x d2y = M A + RA x dx 2 dy 1 EI = M A x + RA x 2 + C1 dx 2 1 1 EIy = M A x 2 + RA x3 + C1x + C2 2 6 EI 1 L< x<L: 2 1 M = M A + RA x − P x − L 2 EI d2y 1 = M = M A + RA x − P x − L 2 dx 2 2 EI dy 1 1 1 = M A x + RA x 2 − P x − L + C3 dx 2 2 2 3 L 1 1 1 EIy = M A x 2 + RA x3 − P x − + C3 x + C4 2 6 6 2 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEMA 9.26 (Continua) dy x = 0, dx = 0 [ x = 0, 0 + 0 + C1 = 0 C1 = 0 y = 0 ] 0 + 0 + 0 + C2 = 0 C2 = 0 L dy dy x = 2 , dx = dx 1 1 1 1 M A L + RA L2 + 0 = M A L + RA L2 − 0 + C3 2 8 2 8 C3 = 0 L x = 2 , y = y 1 1 1 1 M A L2 + RA L3 + 0 + 0 = M A L2 + RAL3 − 0 + 0 + C4 C4 = 0 8 48 8 48 [ x = L, y = 0] 1 1 1 M A L2 + RA L3 − PL3 + 0 + 0 = 0 2 6 48 1 1 3 1 1 3 PL3 = 0 RB L − P L + ( P − RB ) L − 2 2 6 48 RB = 5 P↑ 16 5 P 16 RA = 7 P↑ 16 5 1 PL − PL 16 2 MA = − 3 PL 16 MC = 5 PL 32 RA = P − MA = L 5 L M C = RB = P 2 16 2 MB = 0 Bending moment diagram PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.27 SOLUTION Reactions are statically indeterminate. 0< x< EI L 2 d2y = M = RA x dx 2 EI (1) dy 1 = RA x 2 + C1 dx 2 EIy = (2) 1 RA x3 + C1x + C2 6 (3) L < x< L 2 EI d2y 1 L = M = RA x − w x − 2 2 dx 2 2 (4) 3 EI dy 1 1 L = RA x 2 − w x − + C3 6 2 dx 2 (5) 4 EIy = [ x = 0, y = 0] 1 1 L R A x3 − w x − + C3 x + C4 6 24 2 0 = 0 + 0 + C2 C2 = 0 2 2 L dy dy x = 2 , dx = dx 1 1 L L RA + C1 = RA + 0 + C3 2 2 2 2 L x = 2 , y = y L L 1 L 1 L RA + C1 + C2 = RA − 0 + C3 + C4 2 2 6 2 6 2 dy x = L, dx = 0 1 1 L Rx L2 − w + C3 = 0 2 6 2 [ x = L, 1 1 L 1 1 RAL2 − w + wL3 − RA L2 L + 0 = 0 6 24 2 48 2 y = 0] (6) 3 C1 = C3 3 3 C3 = C2 = C4 = 0 1 1 wL3 − RA L2 48 2 4 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEMA 9.27 (Continua) 1 4 1 1 3 1 2 − 6 RA L = 48 − 384 wL From (1), with x = L , 2 1 7 RA = wL 3 384 RA = 7 L M C = RA = wL2 2 256 7 wL ↑ 128 M C = 0.02734 wL2 2 From (4), with x = L, MB 1 L 1 9 7 = RA L − w = − wL − wL2 2 2 128 128 8 M B = − 0.07031wL Location of maximum positive M: L < x< L 2 L Vm = RA − w xm − = 0 2 xm = From (4), with x = xm , xm − L R 7 = A = L 2 w 128 L 7 71 + L= L 2 128 128 M m = RA xm − 1 L w xm − 2 2 2 7 71 1 7 = wL L − w L 128 128 2 128 2 M m = 0.02884 wL2 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.28 SOLUTION Reactions are statically indeterminate. ΣFy = 0 : RA + RB − w0 L =0 4 RB = w0 L − RA 4 w L 2L ΣM B = 0 : − RA L + 0 + MB = 0 4 3 0≤ x ≤ w= M B = RA L − L ≤ x≤ L: 2 L : 2 2w0 x L M = RA x − w0 2 x L w M = RA x − 0 x 3 3L V = RA − EI d2y w = RA x − 0 x 3 2 3L dx 1 1 w0 4 dy EI x + C1 = RA x 2 − 2 12 L dx 1 1 w0 5 EIy = RA x3 − x + C1x + C2 6 60 L w0 L L x − 4 3 d2y 1 1 L = RA x − w0 L x − 2 12 dx 4 EI EI [ x = 0, y = 0] : 0 = 0 − 0 + 0 + C2 w0 L2 6 dy 1 1 1 Lx + C3 = RA x 2 − w0 L x 2 − dx 2 12 8 EIy = 1 1 1 RA x3 − w0 L x3 − Lx 2 + C3 x + C4 6 24 24 ∴ C2 = 0 L dy dy 1 1 1 1 1 2 3 2 3 x = 2 , dx = dx : 8 RA L − 192 w0 L + C1 = 8 RA L + 96 w0 L + C3 ∴ C3 = C1 − 64 w0 L L 1 1 1 3 4 x = 2 , y = y : 48 RA L − 1920 w0 L + 2 C1L + 0 = 1 1 3 1 3 RA L3 − w0 L L − L 48 96 192 1 L + C1 − w0 L3 + C4 64 2 ∴ C4 = 1 w0 L4 480 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEMA 9.28 (Continua) dy 1 2 1 1 1 1 2 2 2 3 x = L, dx = 0 : 2 RA L − w0 L 8 L − 12 L + C3 = 0 ∴ C3 = − 2 RA L + 24 w0 L [ x = L, y = 0] : Over 1 1 3 1 1 1 1 RA L3 − w0 L L3 − L + − RA L2 + w0 L3 ( L) + w0 L4 = 0 6 24 2 24 480 24 RB = w0 L 21 − w0 L 4 160 MB = 21 w L2 w0 L2 − 0 160 6 0< x< 21 w0 L ↑ 160 RB = 19 w0 L ↑ 160 17 w0 L2 = −0.0354w0 L2 480 L w 21 w , V = RA − 0 x 2 = w0 L − 0 x 2 2 L 160 L V = 0 at M = MB = − RA = x = xm = 0.36228L 21 w w0 Lx − 0 x3 160 3L M A = M ( x = 0) = 0 L M C = M x = = 0.0240w0 L2 2 M m = M ( xm = 0.36228L) = 0.0317 w0 L2 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.29 SOLUTION Reactions are statically indeterminate. ΣFy = 0: RA + 1 1 wL − wL + RB = 0 RA = − RB 2 2 1 L ΣM A = 0: − M A − wL + RB L = 0 2 2 M A = RB L − 0< x≤ From A to C: 1 2 wL 4 L 2 d2y 1 = M = M A + RA x + wx 2 2 2 dx 1 1 dy EI = M A x + RA x 2 + wx3 + C1 2 6 dx 1 1 1 EIy = M A x 2 + RA x3 + wx 4 + C1x + C2 2 6 24 EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEMA 9.29 (Continua) From C to B: L ≤ x< L 2 d2y 1 L 1 L EI 2 = M = M A + RA x + wL x − − w x − 2 4 2 2 dx 2 2 3 dy 1 1 L 1 L EI = M A x + RA x 2 + wL x − − w x − + C3 dx 2 4 4 6 2 3 4 1 1 1 L 1 L EIy = M A x 2 + RA x3 + wL x − − w x − + C3 x + C4 2 6 12 4 24 2 dy x = 0, dx = 0 0 + 0 + 0 + C1 = 0 C1 = 0 [ x = 0, y = 0] 0 + 0 + 0 + 0 + C2 = 0 C2 = 0 L dy dy x = 2 , dx = dx 2 MA 3 L 1 L 1 L L 1 L − RA + w = M A + RA 2 2 6 2 2 2 2 2 2 2 + 1 L wL − 0 + C3 4 4 1 3 1 1 3 C3 = − wL = 192 wL 48 64 L x = 2 , y = y 2 3 1 1 L 1 L L M A + RA + w 2 6 2 24 2 2 2 = 3 4 1 1 L 1 L L M A + RA + wL 2 6 2 12 2 4 −0+ 3 1 L wL3 + C4 192 2 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEMA 9.29 (Continua) 1 1 4 1 1 4 C4 = − − wL = − 768 wL 384 768 384 [ x = L, y = 0] 3 1 1 1 1 L 3L M A L2 + RA L3 + wL − w 2 6 12 24 2 4 + 4 1 1 wL3 ( L) − wL4 = 0 192 768 1 1 1 1 1 1 4 27 RB L − wL2 L2 + (− RB ) L3 + − + − wL = 0 2 4 6 768 384 192 768 7 4 1 1 1 3 2 − 6 RB L = 8 − 192 wL RA = − RB = − M A = RB L − Deflection at C. 1 17 RB = wL 3 192 RB = 17 wL ↑ 64 17 wL 64 1 2 17 1 2 1 wL = wL2 − wL = 4 64 64 4 L y at x = 2 2 EIyC = 3 1 1 L 1 L L M A + RA + w 2 6 2 24 2 2 2 = 4 3 1 1 1 17 1 L L 2 L w wL + − wL + 2 64 6 64 24 2 2 2 17 1 4 1 1 = − + wL4 wL = − 1024 512 3072 384 4 yC = 1 wL4 ↓ 1024 EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.30 SOLUTION Reactions are statically indeterminate. 0 < x< L 2 d2y 1 = M = RA x − wx 2 2 2 dx dy 1 1 EI = RA x 2 − wx3 + C1 dx 2 6 1 1 EIy = RA x3 − wx 4 + C1x + C2 6 24 EI L < x< L 2 (See free body diagram.) M K = 0: − RA x + wL x − + M = 0 2 4 1 EI L d2y 1 1 = M = RA x − wL x − L 2 2 4 dx 2 EI dy L 1 1 = RA x 2 − wL x − + C3 dx 2 4 4 3 EIy = L 1 1 RA x 3 − wL x − + C3 x + C4 6 12 4 [ x = 0, y = 0] : 0 − 0 + 0 + C2 = 0 L dy dy x = 2 , dx = dx : 1 L 1 L 1 L 1 L RA − w + C1 = RA − wL + C3 2 2 6 2 2 2 4 4 2 3 C1 = C3 + 3 C2 = 0 4 2 2 1 1 1 wL3 − wL3 = C3 + wL3 48 64 192 3 3 1 L 1 1 L 1 L L 1 L L 3 L x = 2 , y = y : 6 RA 2 − 24 w 2 + C3 + 192 wL 2 = 6 RA 2 − 12 wL 4 + C3 2 + C4 C4 = − 1 1 1 1 wL4 + wL4 + wL4 = wL4 384 384 768 768 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEM$ 9.30 (ContinuD dy x = L, dx = 0 : 2 1 1 3L RAL2 − wL + C3 = 0 2 4 4 C3 = 9 1 wL3 − RAL2 64 2 3 [ x = L, y = 0] : 1 1 1 1 3L 9 RA L3 − wL + wL3 − RA L2 L + wL4 = 0 6 12 2 768 4 64 27 1 4 1 1 9 3 2 − 6 RA L = 64 − 768 + 768 wL C3 = 1 41 RA = wL 3 384 41 wL ↑ 128 9 1 41 3 5 wL3 − wL = − wL3 64 2 128 256 C1 = − 5 1 11 wL3 + wL3 = − wL3 256 192 768 L y at x = 2 Deflection at C. yC = wL4 1 41 ⋅ EI 6 128 3 1 1 ⋅ − 24 2 4 11 1 1 ⋅ − ⋅ + 0 768 2 2 1 11 wL4 19 wL4 41 − = − − = 6144 EI 6144 384 1536 EI or RA = yC = 19 wL4 ↓ 6144 EI 3 3 wL4 1 41 1 1 1 5 1 1 ⋅ + ⋅ + yC = ⋅ − EI 6 128 2 12 4 256 2 768 41 1 5 1 wL4 19 wL4 = − − + = − 768 EI 6144 EI 6144 768 512 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.31 SOLUTION Reactions are statically indeterminate. Because of symmetry, [ x = 0, y = 0] [ x = L, y = 0] dy L = 0 and V = 0 at x = . dx 2 L Use portion AC of beam. 0 < x ≤ 2 dy dy x = 0, dx = 0 x = L, dx = 0 L x = 2 , V = 0 L dy x = 2 , dx = 0 dV w = − w = −2 0 x dx L EI dM w = V = − 0 x 2 + RA dx L (1) d2y 1 w0 3 =M =− x + RA x + M A 2 3 L dx (2) EI dy 1 w0 4 1 =− x + RA x 2 + M A x + C1 dx 12 L 2 EIy = − (3) 1 w0 2 1 1 x + RA x3 + M A x 2 + C1x + C2 60 L 6 2 dy x = 0, dx = 0 : 0 = 0 + 0 + 0 + C1 C1 = 0 [ x = 0, y = 0] : 0 = 0 + 0 + 0 + 0 + C2 C2 = 0 L x = 2 , V = 0 : − w0 L + RA = 0 L 2 L dy x = 2 , dx = 0 : − 1 w0 L 11 L L + w0 L + M A + 0 = 0 12 L 2 24 2 2 2 4 RA = (4) wL 4 2 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEM$ 9.3 (ContinuD 1 5 1 2 2 M A = −2 − w0 L = − 96 w0 L 32 192 From (2), with x = M A = −0.05208w0 L2 L , 2 3 MC = − 1 w0 L 1 L 5 w0 L12 + w0 L − 3 L 2 4 2 96 1 5 1 1 = − + − w0 L2 = w0 L2 32 24 8 96 M C = 0.03125w0 L2 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.40 SOLUTION Loading I: Case 6 in Appendix D. yC = − Loading II: 5wL4 384EI θA = − wL3 24EI Case 7 in Appendix D. 3 M A L 1 M A L2 L yC = − − L2 = 6EIL 2 2 16 EI MA = with Loading III: wL2 12 yC = θA = 1 M B L3 16 EI M L θA = B 6EI MB = with wL2 12 1 wL3 36 EI (using Loading II result) yC = 1 wL4 192 EI θA = 1 wL3 72 EI Deflection at C. yC = − 5 wL4 1 wL4 1 wL4 1 wL4 + + =− 384 EI 192 EI 192 EI 384 EI yC = (b) M AL 3EI Case 7 in Appendix D. yC = (a) 1 wL4 192 EI θA = 1 wL4 ↓ 384 EI Slope at A. θA = − 1 wL3 1 wL3 1 wL3 + + =0 24 EI 36 EI 72 EI θ A = 0 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.41 SOLUTION Units: Forces in kN; lengths in m. Loading I: Concentrated load at B Case 1 of Appendix D applied to portion AB. θ B′ = − PL2 (3)(0.75) 2 0.84375 =− =− 2EI 2EI EI y′B = − PL3 (3)(0.75)3 0.421875 =− =− 3EI 3EI EI Portion BC remains straight. θC′ = θ B′ = − 0.84375 EI yC′ = y′B − (0.5)θ B′ = − Loading II: Concentrated load at C. 0.84375 EI Case 1 of Appendix D. θ ′′A = − PL2 (3)(1.25) 2 2.34375 =− =− 2EI 2 EI EI y′′A = − PL3 (3)(1.25)3 1.953125 =− =− EI 3EI 3EI 3.1875 EI 2.796875 y A = y′A + y′′A = − EI By superposition, θ A = θ ′A + θ A′′ = − Data: E = 200 × 109 Pa, I = 2.52 × 106 mm 4 = 2.52 × 10−6 m 4 EI = (200 × 104 )(2.52 × 10−6 ) = 504 × 103 N ⋅ m 2 = 504 kN ⋅ m 2 Slope at C. θC = − 3.1875 = −6.32 × 10−3 rad 504 Deflection at C. yC = − 2.796875 = −5.55 × 10−3 m 504 θC = 6.32 × 10−3 rad yC = 5.55 mm ↓ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.42 SOLUTION Units: Forces in kN; lengths in m. The slope and deflection at B depend only on the deformation of portion AB. Reduce the force at C to an equivalent force-couple system at B and add the force already at B to obtain the loadings I and II shown. Loading I: Loading II: Case 1 of Appendix D. θ B′ = − PL2 (6)(0.75) 2 1.6875 =− =− 2EI 2 EI EI y′B = − PL3 (6)(0.75)3 0.84375 =− =− EI 3EI 3EI Case 3 of Appendix D. θ B′′ = − ML (1.5)(0.75) 1.125 =− =− EI EI EI y′′B = − (1.5)(0.75)2 0.421875 ML2 =− =− 2EI EI EI By superposition, 2.8125 EI 1.265625 yB = y′B + y′′B = − EI θ B = θ B′ + θ B′′ = − Data: E = 200 × 109 Pa, I = 2.52 × 106 mm 4 = 2.52 × 10−6 m 4 EI = (200 × 109 )(2.52 × 10−6 ) = 504 × 103 N ⋅ m 2 = 504 kN ⋅ m 2 Slope at B. θB = − 2.8125 = −5.58 × 10−3 rad 504 Deflection at B. yB = − 1.265625 = −2.51 × 10−3 m 504 θ B = 5.58 × 10−3 rad yB = 2.51 mm ↓ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.45 SOLUTION Units: Forces in kN; lengths in m. Loading I: Moment at B. M = 80 kN ⋅ m, L = 5.0 m, x = 2.5 m Case 7 of Appendix D. ML (80)(5.0) 66.667 = = 6 EI 6 EI EI M 80 125 yC = − ( x3 − L2 x) = − [2.53 − (5.0)2 (2.5)] = EI 6 EIL 6 EI (5.0) θA = Loading II: Moment at A. Case 7 of Appendix D. M = 80 kN ⋅ m, L = 5.0 m, x = 2.5 m ML (80)(5.0) 133.333 θA = = = 3EI 3EI EI yC = Loading III: 125 EI 140 kN concentrated load at C. (Same as loading I.) P = 140 kN PL2 (140)(5.0)2 218.75 =− =− 16 EI 16 EI EI PL3 (140)(5.0)3 364.583 =− =− yC = − 48 EI 48 EI EI θA = − E = 200 × 109 Pa, I = 156 × 106 mm 4 = 156 × 10−6 m 4 Data: EI = (200 × 109 )(156 × 10−6 ) = 31.2 × 106 N ⋅ m 2 = 31200 kN ⋅ m 2 (a) Slope at A. θA = 67.667 + 133.333 − 218.75 = −0.601 × 10−3 rad 31200 θ A = 0.601 × 10−3 rad (b) Deflection at C. yC = 125 + 125 − 364.583 = −3.67 × 10−3 m 31200 yC = 3.67 mm ↓ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.46 SOLUTION Units: Forces in kN; lengths in m. Loading I: 8 kN/m uniformly distributed. Case 6: w = 8 kN/m, L = 3.9 m, x = 1.3 m WL3 (8)(3.9)3 19.773 =− =− 24 EI 24EI EI w 8 yC = − [ x 4 − 2Lx3 + L3 x] = − [(1.3) 4 − (2)(3.9)(1.3)3 + (3.9)3 (1.3)] 24EI 24 EI 20.945 =− EI θA = − Loading II: 35 kN concentrated load at C. Case 5 of Appendix D. P = 35 kN, L = 3.9 m, a = 1.3 m, b = 2.6 m, x = a = 1.3 m Data: θA = − Pb( L2 − b 2 ) (35)(2.6)(3.92 − 2.6) 2 32.861 =− =− 6EIL 6EI (3.9) EI yC = − Pa 2b 2 (35)(1.3) 2 (2.6) 2 34.176 =− =− 3EIL 3EI (3.9) EI E = 200 × 109 , I = 102 × 106 mm 4 = 102 × 10−6 m 4 EI = (200 × 109 )(102 × 10−6 ) = 20.4 × 106 N ⋅ m 2 = 20, 400 kN ⋅ m 2 (a) Slope at A. θA = − θ A = 2.58 × 10−3 rad (b) 19.773 + 32.861 = −2.58 × 10−3 rad 20, 400 Deflection at C. yC = − 20.934 + 34.176 = −2.70 × 10−3 m 20, 400 yC = 2.70 mm ↓ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.48 SOLUTION Consider RC as redundant and replace loading system by I and II. Loading I: (Case 4 of Appendix D.) Loading II: (Case 7 of Appendix D.) yC′ = − RC L3 48 EI yC′′ = − = 3 M 0 L L − L2 6 EIL 2 2 M 0 L2 16 EI Superposition and constraint: yC = yC′ + yC′′ = 0 − RC L3 M 0 L2 + =0 48EI 16 EI 3M 0 L ΣM B = 0: − RA L + − M0 = 0 L 2 ΣFY = 0: M 0 3M 0 − + RB = 0 2L L RC = 3M 0 ↓ L RA = RB = M0 ↑ 2L 5M 0 ↑ 2L PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.49 SOLUTION Beam is indeterminate to first degree. Consider RA as redundant and replace the given loading by loadings I, II, and III. Loading I: Case 1 of Appendix D. ( yA)I = Loading II: RA L3 3EI Case 2 of Appendix D. ( y A ) II = − Loading III: wL4 8EI Case 2 of Appendix D (portion CB). (θC ) III = − ( yC ) III = w( L/2)3 1 wL3 =− 6 EI 48 EI 1 wL4 w( L/2)4 = 8EI 128 EI Portion AC remains straight. ( y A ) III = ( yC ) III + Superposition and constraint: (a) L 7 wL4 (θC ) III = 2 384 EI y A = ( y A ) I + ( y A ) II + ( y A ) III = 0 1 RA L3 1 wL4 7 wL4 1 RA L3 41 wL4 − + = − =0 3 3EI 8 EI 384 EI 3 EI 384 EI RA = 41 wL ↑ 128 RB = 23 wL ↑ 128 Statics: (b) ΣFy = 0 : 41 1 wL − wL + RB = 0 128 2 41 1 3L wL L − wL − M B = 0 ΣM B = 0 : − 128 2 4 MB = 7 wL2 128 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.50 SOLUTION Consider RA as redundant and replace loading system by I and II. y ′A = Loading I: (Case 1 of Appendix D.) Loading II: Portion BC. (Case 3 of Appendix D.) yC′′ = − M 0 ( L − a)2 2 EI θC′′ = M 0 ( L − a) EI y ′′A = yC′′ − (a)θC Portion AC is straight. =− (a) RA L3 3EI Superposition and constraint: M 0 ( L − a) 2 aM 0 ( L − a ) − 2 EI EI y A = y ′A + y ′′A = 0 RA L3 M 0 ( L − a) 2 aM 0 ( L − a) − − =0 3EI 2 EI EI 2 RA L3 − M 0 ( L − a)( L − a + 2a ) = 0 3 2 RA L3 = M 0 ( L2 − a 2 ) 3 (b) ΣFy = 0: RA + RB = 0 RB = − RA ΣM B = 0: M B + M 0 − RA L = 0 MB = RA = 3M 0 2 2 L − a 2 − L2 2 3 2L RB = MB + M0 − 3M 0 2 L3 3M 0 2 L3 ( L2 − a 2 ) ↑ ( L2 − a 2 ) ↓ 3 M0 2 (L − a2 ) = 0 2 L2 MB = M0 2 L2 ( L2 − 3a 2 ) PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.51 SOLUTION Beam is second degree indeterminate. Choose RB and M B as redundant reactions. Loading I: Case 1 of Appendix D. ( yB ) I = Loading II: RB L3 3EI (θ B ) I = RB L2 2EI Case 3 of Appendix D. ( yB ) II = − M B L2 2 EI (θ B ) II = − M BL EI Loading III: Case 2 of Appendix D. ( yB ) III = − wL4 8EI (θ B ) III = − wL2 6 EI Superposition and constraint: yB = ( yB ) I + ( yB )II + ( yB ) III = 0 L3 L2 wL4 RB − MB − =0 3EI 2EI 8EI (1) θ B = (θ B ) I + (θ B ) II + (θ B ) III = 0 L2 L wL3 =0 RB − MB − 2EI 6EI EI (2) Solving Eqs. (1) and (2) simultaneously, RB = MB = 1 wL ↑ 2 1 wL2 12 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.52 SOLUTION Beam is second degree indeterminate. Choose RB and M B as redundant reactions. Loading I: Case 1 of Appendix D. ( yB ) I = − Loading II: RB L3 R L2 , (θ B ) I = − B 3EI 2 EI Case 3 of Appendix D. ( yB ) II = M B L2 M L , (θ B )II = B EI 2 EI Loading III: Case 3 applied to portion AC. M 0 ( L/2) 2 M 0 L2 = 2 EI 8 EI M 0 ( L/2) M 0 L = = 2 EI EI ( yC )III = (θC )III Portion CB remains straight. 3 M 0 L2 L (θC ) III = 2 8 EI 2 1 M0L = 2 EI ( yB ) III = ( yC ) III + (θ B ) III = (θC )III Superposition and constraint: yB = ( yB ) I + ( yB )II + ( yB ) III = 0 − L3 L2 3 M 0 L2 RB + MB + =0 3EI 2 EI 8 EI (1) θ B = (θ B ) I + (θ B ) II + (θ B ) III = 0 − L2 L 1 M0L RB + MB + =0 EI 2 EI 2 EI (2) Solving Eqs. (1) and (2) simultaneously, RB = 3 M0 ↓ 2 L MB = 1 M0 4 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.53 SOLUTION Let a = 0.4 m. Cantilever beams AB and CD. Cases 1 and 2 of Appendix D. yB = yD = − ( wa) a3 wa 4 11 wa 4 − =− 3EI 8EI 24 EI Beam BCD, with L = 0.8 m, assuming that points B and D do not move. Case 6 of Appendix D. yC′ = − 5wL4 384 EI Additional deflection due to movement of points B and D. yC′′ = yB = yD = − Total deflection at C. yC = yC′ + yC′′ yC = − Data: 11 wa 4 24 EI w EI 4 4 5L 11a + 24 384 E = 200 × 109 Pa, 1 I = (24)(12)3 = 3.456 × 10−3 mm 4 = 3.456 × 10−9 m 4 12 EI = (200 × 109 )(3.456 × 10−9 ) = 691.2 N ⋅ m 2 yC = −3 × 10−3 m −3 × 10−3 = − w (5)(0.8) 4 (11)(0.4) 4 −6 + = −24.69 w 691.2 384 24 w = 121.5 N/m PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.56 SOLUTION Units: Forces in kN; lengths in m. Using free body ABC, M A = 0: 4.4 RC − (4.4)(30)(2.2) = 0 RC = 66.0 kN E = 200 × 109 Pa I = 125 × 106 mm 4 = 125 × 10−6 m 4 EI = (200 × 109 )(125 × 10−6 ) = 25.0 × 10−6 N ⋅ m 2 = 25,000 kN ⋅ m 2 For slope and defection at C, use Case 1 of Appendix D applied to portion CE of beam DCE. θC = RC L2 (66.0)(2.2) 2 = = 6.3888 × 10−3 rad 2EI (2)(25, 000) yC = − RC L3 (66.0)(2.2)3 = = −9.3702 × 10−3 m 3EI (3)(25, 000) Defection at B, assuming that point C does not move. Use Case 6 of Appendix D. ( yB )1 = − 5WL4 (5)(30)(4.4) 4 =− = −5.8564 × 10−3 384EI (384)(25, 000) Additional defection at B due to movement of point C: (a) Total deflection at B. ( yB ) 2 = 1 yC = −4.6851 × 10−3 m 2 yB = ( yB )1 + ( yB )2 = −10.54 × 10−3 m yB = 10.54 mm ↓ Portion DC of beam DCB remains straight. (b) Deflection at D. yD = yC − aθC = −9.3702 × 10−3 − (2.2)(6.3888 × 10−3 ) = −23.4 × 10−3 m yD = 23.4 mm ↓ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.58 SOLUTION Let P be the tension developed in member AB and δ B be the elongation of that member. A = 255 mm 2 = 255 × 10−6 m 2 Cable AB: δB = PL ( P)(3) = EA (200 × 109 )(255 × 10−6 ) = 58.82 × 10−9 P I = 156 × 106 mm 4 = 156 × 10−6 m 4 Beam BC: EI = (200 × 109 )(156 × 10−6 ) = 31.2 × 106 N ⋅ m 2 Loading I: 20 kN/m downward. Refer to Case 2 of Appendix D. ( yB )1 = − wL4 (20 × 103 )(6) 4 =− 8EI (8)(31.2 × 106 ) = −103.846 × 10−3 m Loading II: Upward force P at Point B. Refer to Case 1 of Appendix D. ( yB ) 2 = PL3 P(6)3 = = 2.3077 × 10−6 P 3EI (3)(31.2 × 106 ) yB = ( yB )1 + ( yB ) 2 By superposition, Also, matching the deflection at B, yB = −δ B −103.846 × 10−3 + 2.3077 × 10−6 P = −58.82 × 10−9 P 2.3666 × 10−6 P = 103.846 × 10−3 P = 43.9 × 103 N P = 43.9 kN PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.59 SOLUTION Let length AB = L = 0.5 m length BC = a = 0.2 m Consider portion AB of beam ABC. The loading becomes forces P and RB at B plus the couple Pa. The deflection at B is δ 0. Using Cases 1 and 3 of Appendix D, δ0 = ( P − RB ) L3 PaL2 + 3EI 2 EI L3 L2a L3 + RB = EI δ 0 P − 2 3 3 (1) The deflection at C depends on the deformation of beam ABC subjected to loads P and RB . For loading I, using Case 1 of Appendix D, (δ C )1 = P ( L + a )3 3EI For loading II, using Case 1 of Appendix D, yB = RB L3 3EI θB = RB L2 2EI Portion BC remains straight. L3 L2a RB + yC = yB + aθ B = 2 EI 3 By superposition, the downward deflection at C is δC = P( L + a)3 L3 L2a RB − + 3EI 2 EI 3 L3 L2a ( L + a)3 P − + RB = EI δ C 3 2 3 (2) PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEM$ 9. (ContinuD Data: E = 200 × 109 Pa I = 1 (60)(60)3 = 1.08 × 106 mm 4 = 1.08 × 10−6 m 4 12 EI = 216 × 103 N ⋅ m 2 δ 0 = 0.5 × 10−3 m δ C = 1.0 × 10−3 m Using the data, eqs (1) and (2) become 0.06667 P − 0.04167 RB = 108 (1)′ 0.11433 P − 0.06667 RB = 216 (2)′ Solving simultaneously, P = 5.63 × 103 N P = 5.63 kN ↓ RB = 6.42 × 103 N PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.62 SOLUTION Let 200 N = P. Consider torsion of rod AB. TL ( PL) L PL2 = = JG JG JG PL3 yC′ = − LφB = − JG φB = Consider bending of AB. (Case 1 of Appendix D.) yC′′ = yB = − PL3 3EI Consider bending of BC. (Case 1 of Appendix D.) yC′′′ = − PL3 3EI Superposition: yC = yC′ + yC′′ + yC′′′ =− PL3 PL3 PL3 PL3 EI 2 − − =− + JG 3EI 3EI EI JG 3 Data: G = 80(109 ) Pa E = 200(109 ) Pa EI = 643.40 N ⋅ m 2 yC = − 1 J = π (0.008) 4 = 6.4340(10−9 ) m 4 2 1 I = J = 3.2170(10−9 ) m 4 2 JG = 514.72 N ⋅ m 2 (200)(0.25)3 643.40 2 + = −9.3093(10−3 ) m 643.40 514.72 3 yC = 9.31 mm ↓ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.63 SOLUTION w( x) = 2w0 x − w0 L w 2w V ( x) = − w( x)dx = − 0 x − w0 dx = − 0 x 2 + w0 x + C1 L L [ x = 0, V = 0] 0 = 0 + 0 + C1 ∴ C1 = 0 w w w M ( x) = V ( x)dx = − 0 x 2 + w0 x dx = − 0 x3 + 0 x 2 + C2 L 3 L 2 [ x = 0, M = 0] 0 = 0 + 0 + C2 ∴ C2 = 0 w w d2y = M = − 0 x3 + 0 x 2 2 3 2 L dx w w dy EI = − 0 x 4 + 0 x3 + C3 dx 12 L 6 EI x = L, w L3 w L3 dy = 0 0 = − 0 + 0 + C3 dx 12 6 EIy = − Elastic curve. (b) y at x = 0. (c) dy at x = 0. dx w0 L4 w0 L4 w0 L4 + − + C4 60 24 12 y=− yA = + dy dx =− A w0 L3 12 w0 5 w0 4 w0 L3 x + x − x + C4 60 L 24 12 [ x = L, y = 0] 0 = − (a) ∴ C3 = − 7 w0 L4 120 EI w0 L3 12 EI ∴ C4 = 7 w0 L4 120 w0 (2 x5 − 5 Lx 4 + 10 L4 x − 7 L5 ) 120 EIL yA = θA = 7 w0 L4 ↑ 120 EI w0 L3 12 EI PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.68 SOLUTION M C = 0: − 4.5RA + (20)(3)(1.5) − (60)(1.5) = 0 RA = 0 Forces in kN; lengths in m. Units: 1 d2y 1 0 2 = M = 60 x − 1.5 − 90 x − 1.5 − (20) x − 1.5 2 2 dx dy 1 EI = 30 x − 1.5 2 − 90 x − 1.51 − (20) x − 1.5 3 + C1 dx 6 EI EIy = 10 x − 1.5 3 − 45 x − 1.5 2 − 1 (20) x − 1.5 4 24 + C1x + C2 Boundary conditions: Data: [ x = 0, y = 0] 0 + 0 + 0 + 0 + C2 = 0 [ x = 4.5, y = 0] (10)(3)3 − (45)(3) 2 − 1 (20)(3)4 + 4.5C1 + 0 = 0 24 C2 = 0 C1 = 45 kN ⋅ m 2 E = 200 × 109 Pa, I = 316 × 106 mm 4 = 316 × 10−6 m 4 EI = (200 × 109 )(316 × 10−6 ) = 63.2 × 106 N ⋅ m 2 = 63, 200 kN ⋅ m 2 (a) Slope at A. dy dx at x = 0 EIθ A = C1 = 45 kN ⋅ m 2 θA = (b) 45 = 0.712 × 10−3 rad 63, 200 θ A = 0.712 × 10−3 rad ( y at x = 1.5) Deflection at B. EIyB = (C1)(1.5) = (45)(1.5) = 67.5 kN ⋅ m3 yB = 67.5 = 1.068 × 10−3 m 63, 200 yB = 1.068 mm ↑ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.69 SOLUTION 1 (50)(50)3 = 520.833 × 103 mm3 = 520.833 × 10−9 m 12 EI = (105 × 109 )(520.833 × 10−6 ) = 54.6875 × 103 N ⋅ m 2 I= = 54.6875 kN ⋅ m 2 Units: Forces in kN; lengths in meters. Compute deflection at B due to w. Case 8 of Appendix D. ( yB )1 = − wL4 (30)(0.400) 4 =− 8 EI (8)(54.6875) = −1.75543 × 10−3 = −1.7553 mm The displacement is more than δ 0 , the gap closes. Let P be the contact force between points B and C. Compute deflection of B due to P. Use Case 1 of Appendix D. ( yB )2 = PL3 P(0.4)3 = 3EI (3)(54.6875) = 390.095 × 10−6 P m Compute deflection of C due to P. yC = − PL3 P (0.25)3 =− = −95.238 × 10−6 P 3EI (3)(54.6875) m Displacement condition: yB + δ 0 = yC Using superposition, ( yB )1 + ( yB )2 − δ 0 = yC −1.75543 × 10−3 + 390.095 × 10−6 P + 1.2 × 10−3 = −95.238 × 10−6 P 485.333 × 10−6 P = 0.55543 × 10−3 P = 1.14443 kN PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEM$ 9. (ContinuD (a) Reaction at A. ΣFy = 0: RA − 12 + 1.14443 = 0 RA = 10.86 kN ↑ ΣM A = 0: M A − (0.2)(12) + (0.4)(1.14443) = 0 M A = 1.942 kN ⋅ m (b) Reaction at D. ΣFy = 0: RD − 1.14443 = 0 RD = 1.144 kN ↑ ΣM D = 0: −M D + (0.25)(1.14443) = 0 M D = 0.286 kN ⋅ m PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.70 SOLUTION Units: Forces in kN; lengths in m. E = 200 × 109 Pa I = 40.1 × 106 mm 4 = 40.1 × 10−6 m 4 EI = (200 × 109 )(40.1 × 10−6 ) = 8.02 × 106 N ⋅ m 2 = 8020 kN ⋅ m 2 Draw M/EI diagram by parts. M1 (18)(2.2) = = 4.9377 × 10−3 m −1 EI 8020 1 A1 = (4.9377 × 10 −3 )(2.2) = 5.4315 × 10−3 2 1 x1 = (2.2) = 0.7333 m 3 M2 (26)(2.7) 2 =− = −11.8167 × 10−3 m −1 EI (2)(8020) 1 (−11.8167 × 10−3 )(2.7) = −10.6350 × 10−3 3 1 x2 = (2.7) = 0.675 m 4 A2 = Draw reference tangent at C. θC = θ A + θC / A = θ A + A1 + A2 = 0 (a) Slope at A. θ A = − A1 − A2 = −5.4315 × 10−3 + 10.6350 × 10−3 = 5.20 × 10−3 rad θ A = 5.20 × 10−3 rad PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl PROBLEM$ 9. (ContinuD (b) Deflection at A. y A = yC − θC L + t A / C = 0 − 0 + A1x1 + A2 x2 = 0 − 0 + (5.4315 × 10−3 )(1.9667) − (10.6350 × 10−3 )(2.025) = −10.85 × 10−3 m y A = 10.85 mm ↓ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.71 SOLUTION For W130 × 23.8, I x = 8.91 × 106 mm 4 EI = (200 × 106 kPa)(8.91 × 10−6 m 4 ) = 1782 kN ⋅ m 2 Let RB be the jack force in kN. 1 (1.8 RB )(1.8) = 1.62 RB 2 1 A2 = (−60)(3) = −90 kN ⋅ m 2 2 EI tC / A = (2.4) A1 + (2) A2 A1 = 0 = (2.4)(1.62 RB ) + (2)(−90) RB = 46.296 kN A1 = 75 kN ⋅ m 2 1 (−60)(1.8) = −54 kN ⋅ m 2 2 1 A4 = (−24)(1.8) = −21.6 kN ⋅ m 2 2 EIt B/A = (1.2) A1 + (1.2) A3 + (0.6) A4 A3 = = (1.2)(75) + (1.2)(−54) + (0.6)(−21.6) = 12.24 kN ⋅ m 2 (a) Deflection at B. (b) Reaction at B. yB = tB / A = EI t B / A 12.24 = = 6.8687 × 10−3 m EI 1782 yB = 6.87 mm ↑ RB = 46.3 kN ↑ PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission. F. P. Beer et al., Meccanica dei solidi, Elementi di scienza delle costruzioni, 5e - isbn 9788838668579, © 2014 McGraw-Hill Education (Italy) srl Esercizio 9.74 SOLUTION Symmetric beam and loading: Spring force: RC = RA 1 2 F = (2wL) = wL 3 3 ΣFy = 0: RA + F − 2wL + RC = 0 RA = RC = 2 wL 3 Draw M/EI diagram by parts. A1 = 1 2 wL2 1 wL3 L = 2 3 EI 3 EI 1 1 wL2 1 wL3 A2 = − L = − 3 2 EI 6 EI Place reference tangent at B. θB = 0 yB = −t A/B 2 3 = − A1 ⋅ L + A2 ⋅ L 3 4 =− 7 wL4 72 EI F = − kyB k=− F = yB 2 wL 3 7 wL4 72 EI k= 48 EI 7 L3 PROPRIETARY MATERIAL. © 2012 The McGraw-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed, reproduced, or distributed in any form or by any means, without the prior written permission of the publisher, or used beyond the limited distribution to teachers and educators permitted by McGraw-Hill for their individual course preparation. A student using this manual is using it without permission.
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