Solutions to problems Structural Stability Theory and Practice by Sukhvarsh Jerath
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Solutions to exercises for Structural Stability Theory and Practice by Sukhvarsh Jerath
Solutions to problems Structural Stability Theory and Practice by Sukhvarsh Jerath
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You can access complete document on following URL. Contact me if site not loaded https://solumanu.com/product/structural-stability-theory-and-practice-jerath/ smtb98@gmail.com Solution Manual Structural Stability Theory and Practice Buckling of Columns, Beams, Plates, and Shells 1 Contact me in order to access the whole complete document - Email: smtb98@gmail.com WhatsApp: https://wa.me/message/2H3BV2L5TTSUF1 - Telegram: https://t.me/solutionmanual
PROBLEMS 1.1 Find the critical load Pcr for the rigid bar column in Fig. P1.1 by using the equilibrium method. The column is restricted by a rotational spring of stiffness c at the support. c P L A B Fig. P1.1 M 0 PL sin θ – cθ = 0 or c P L For small deformation, sin θ ≈ θ c P L A sin cr 2
1.2 Solve problem 1.1 by the energy method. 1 2 2 U c V PL 1 cos 1 2 2 U V c PL 1 cos d d 0 For equilibrium, or c For small deformations, sin θ ≈ θ or c P L PL sin 0 cr 3
1.3 Determine the critical load Pcr for the rigid bar column in Figs. P 1.3 a and b by using the equilibrium method. P P k2 L L k k1 45o (a) (b) Fig. P 1.3 (a) M 0 PL A sin k AD 0 BC BC 2 L cos L 2 4 2 δ = Extension of the spring AD L sin 4 2 PL sin k 2 cos L L 2 L sin 0 4 2 4 2 4
or 2 PL sin 2 kL cos cos sin sin sin cos cos sin 4 2 4 2 4 2 4 2 2 2 kL sin cos cos sin 0 + 4 2 4 2 or 2 2 PL sin kL cos2 kL cos sin 0 2 2 cos2 cos sin 2 2 P kL sin If θ is small, cos θ ≈ 1, sin θ ≈ θ kL P cr 2 (b) M sin F k For small deformations, sin θ ≈ θ, cos θ ≈ 1 2( ) PL k L L 2( ) 0 k k L or 2 2 2 ( k L k k 0 PL k A k ( L sin ) cos L 0 (1) 0 L 2 horizontal 2( sin ) 0 (2) 1 0 1 0 0 k L PL k L ) 2 1 2 2 k L PL k L 2 2 0 k L ( k k ) 2 1 2 5
or ( or 2 2 2 2 k k )( k L PL ) k L 0 1 2 2 1 2 k k P L cr k k 1 2 6
1.4 Solve Problem 1.3 by energy method. (a) 1 2 1 2 2 U k 2 2 2 2 U k 4 L cos 2 L 4 L 2cos 4 2 4 2 V=-PL(1-cos θ) U or 1 2 V 2 2 2 2 k 4 L cos 2 L 4 L 2cos PL (1 cos ) 4 2 4 2 d d 0 For equilibrium, d d or d d or 1 2 1 2 1 2 2 2 k 4 L (2)cos sin 4 L 2sin PL sin 0 4 2 4 2 4 2 1 2 2 2 k 2 L cos sin cos sin 2 L cos sin PL sin 0 2 2 2 2 2 2 kL cos2 cos sin 2 2 P sin For small θ, cos θ ≈ 1, sin θ ≈ θ kL P cr 2 d d d d At θ = 0 2 d d 2cos2 kL 1 2 cos sin PL sin 2 1 2 2 2 2 kL 2sin2 sin cos PL cos 2 2 2 1 2 kL 2 kL PL 2 2 d d d P P , 0 For cr 2 2 2 kL P P , 0 When cr 2 2 d Hence, the system is stable for P < Pcr and is unstable for P >Pcr in the initial position. 7
(b) 1 2 1 2 2 2 U k k ( L sin ) 1 2 V = -PL(1-cosθ) 1 2 For equilibrium For small deformations, sin θ ≈ θ and cos θ ≈ 1 1 2 2 2 k k ( L sin ) PL (1 cos ) 1 2 k 2( L sin )( cos ) L PL sin k k 2( L sin ) 1 2 0 0 k L PL k L 2 2 k L k k 2 1 2 These are same equations as in Problem 1.3(b). 1 2 k k P L Hence, cr k k 1 2 2 2 For initial position, θ = δ = 0 2 K 2 K 2 k L sin k L cos2 PL cos 2 2 2 2 k k 1 2 2 2 cos k L 2 k L PL 11 2 2 k k 22 1 2 2 2 K K k L 12 21 2 2 0 Two degrees of freedom system is in stable equilibrium if or D1 = K11 >0, or k2L2 – PL > 0, or P < k2L K K k L D K K or 2 2 2 2 1 2 2 ( )( ) k L PL k k k L k k P L k k 2 PL k L 11 12 2 2 0 or 0 2 k L k k 21 22 2 1 2 0 1 2 or 1 2 This is a sample only. Lat solved problem in chapter1 is #6. 8