________________________________________________________________________ PROBLEMS (12.58 through 12.61) A beam is loaded and supported as shown in Figs. P12.58 through P12.61. Apply Castigliano's theorem to determine the deflection at point C. SOLUTION (12.58) y P x 2a A C a B M0 = 3 Pa 2 Segment CB M1 = M 0 Segment AC M 2 = M 0 − P( x − a) We have: Hence, ∂M 1 ∂P = 0 ∂M 2 ∂P = −( x − a) 3a 3a EIvC = − ∫ M 0 ( x − a)dx + P ∫ ( x 2 − 2ax + a 2 )dx a a 3a 2 3a 2 x x = M 0 − + ax + P − ax 2 + a 2 x 2 3 a a 3Pa 3 1 1 Pa 3 [− (9 − 1) + 2] + Pa 3 [ (27 − 1) − 8 + 2] = − 2 2 3 3 3 Pa vC = ↑ 3EI = or SOLUTION (12.59) Q A RA=Q/2 a x x” w C a x’ B a D RB=2wa+Q/2 Continued on next slide Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful. Segment AC ∂M 1 x 1 M 1 = Qx = 2 ∂Q 2 Let Q=0: ∂M 1 1 a M1 dx = 0 ∫ 0 EI ∂Q Segment CB 1 1 M 2 = Q(a + x ') − Qx '− wx '2 2 2 Q 1 = (a − x ') − wx '2 2 2 ∂M 2 1 = (a − x ') ∂Q 2 Let Q=0: ∂M 2 1 1 a wx '2 1 wa 4 = − − ' ( ) ( ') M dx a x dx = − ' 2 ∂Q EI ∫ EI ∫0 48EI 2 2 Segment BD ∂M 3 1 M 3 = − wx ''2 =0 2 ∂Q Therefore ∂M i wa 4 ↑ vC = ∫ M i dx = ∂Q 48EI Continued on next slide Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful. SOLUTION (12.60) Add force Q at point C as shown in Fig. (a). 2 L M U =∫ dx 0 2 EI ∂U 1 L ∂M = δC = M dx ∂Q EI ∫0 ∂Q Q P x C B L/2 L/2 Figure (a) ∂M =0 ∂Q L M = − Px − Q( x − ), 2 M = − Px, Part AC. Part CB. ∂M L = −( x − ) ∂Q 2 Let Q=0: 1 L2 1 L L (− Px)(0)dx + (− Px)[−( x − )]dx ∫ ∫ 0 L 2 EI EI 2 P L 2 L P 1 3 1 L 3 L 1 2 L 1 L 2 ( x − x)dx = [ L − ( ) −( ) L +( ) ( ) ] = EI ∫L 2 2 EI 3 3 2 2 2 2 2 2 3 5 PL = 48 EI δC = SOLUTION (12.61) Q L/2 A wL 8 C + Q2 wL Q + )x 8 2 L/2 x’ x Segment AC M1 = ( w B 3 wL 8 + Q2 ∂M 1 x = ∂Q 2 Segment CB M2 = ( wx '2 3wL Q + ) x '− 8 2 2 ∂M 2 x ' = ∂Q 2 Let Q=0: L 2 3wLx ' wLx x wx '2 x ' dx + ∫ ( − ) dx ' 0 0 8 2 8 2 2 2 2 L 2 wLx L 2 3wLx ' wx '3 wL4 dx + w∫ ( − )dx ' = = w∫ 0 0 16 16 4 96 Continued on next slide EIvC = ∫ L2 Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful. or wL4 vC = ↓ 96 EI Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.