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OPTIMIZATION OF SHALLOW ARCHES AGAINST SNAP-THROUGH BUCKLING A THESIS ... PDF

205 Pages·2007·21.55 MB·English
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OPTIMIZATION OF SHALLOW ARCHES AGAINST SNAP-THROUGH BUCKLING A THESIS Presented To The Faculty of the Division of Graduate Studies and Research By Hartley McMullin Caldwell, III In Partial Fulfillment of the Requirements for the Degree Doctor of Philosophy in the School of Engineering Science and Mechanics Georgia Institute of Technology March, 1977 OPTIMIZATION OF SHALLOW ARCHES AGAINST SNAP-THROUGH BUCKLING Approved: _ r, r = U George J. Simitses, Chairman C. V. Smith Jl S. Atluri Date Approved by ChairmanMAR 14 1977 This Dissertation is Dedicated To Thornwell, A Home and School for Children Clinton, South Carolina Ill ACKNOWLEDGMENTS Special appreciation is extended to Professor George J. Simitses, the author's thesis advisor, for his patience and encouragement during the course of this inves tigation. The many enlightening discussions and remarkable insights shared with th€> author will always be a constant source of motivation. Thanks are also extended to Professors C. V. Smith, S. Atluri, C. E. S. Ueng and R. L. Carlson who served on the thesis committee and provided invaluable comments and advice. A special note of thanks to Ms. Brenda Smiley and Ms. Barbara Geiger for an excellent job in typing the final manuscript and to Ms. Sharon Flores for her assistance in putting the early drafts into a readable form. And finally, sincere appreciation is extended to my family for whose encouragement and devotion I will be forever indebted. IV TABLE OF CONTENTS Page ACKNOWLEDGMENTS . . . . . . .. iii LIST OF TABLES vi LIST OF ILLUSTRATIONS . vii SUMMARY x NOTATIONS , xiii Chapter I. INTRODUCTION 1 1.1 Statement of Problem 1.2 Historical Review II. MATHEMATICAL FORMULATION 12 2.1 Buckling Analysis 2.2 Development, of Optimality Criteria III. SOLUTION PROCEDURE 34 3.1 Energy Interpretation of the Optimality Criterion 3.2 Optimization for Anti-Symmetric Modes 3.3 Optimization for Symmetric Modes IV. RESULTS AND DISCUSSION 50 4.1 Analysis of Anti-Symmetric Optimal Designs 4.2 Analysis of Symmetric Optimal Designs 4.3 Determination of the Strongest Design V. CONCLUSIONS AND RECOMMENDATIONS 68 5.1 Conclusions 5.2 Recommendations Appendix A. ANALYTIC APPROACH FOR UNIFORM ARCH BUCKLING . 91 V Appendix Page B. FINITE ELEMENT METHOD APPLIED TO BUCKLING OF SHALLOW ARCHES 116 C. ANALYTIC APPROACH FOR ANTI-SYMMETRIC OPTIMIZATION 129 D. DATA GENERATION AND PROGRAM LISTING 140 REFERENCES . . . .. 183 VITA 188 VI LIST OF TABLES Table Page Al. Effect of Rotational Restraint on the Critical Axial Stress, p, and the Lowest Rise Parameter for Anti symmetric Buckling. 107 vii LIST OF ILLUSTRATIONS Figure Page 1. Shallow Arch Geometry and Sign Convention . . .. 71 2. Anti-Symmetric Response of Optimum Shapes for Various Values of n, 3 =°° 72 0 3. Anti-Symmetric Response of Optimum Designs for Various Values of n, 3 = 10.0 73 0 4. Anti-Symmetric Response of Optimum Designs for Various Values of n,B = 0 74 0 5a. Optimum Designs for Various Values of n. Anti-Symmetric Buckling, 3 = °°. 75 5b. Optimum Designs for Various Values of n. Anti-Symmetric Buckling, $ = 0 76 o 5c. Optimum Designs for Various Values of n. Anti-Symmetric Buckling, 3 =10.0 77 6. Critical Load Versus Rise Parameter for T ^ and I , 3 = «, n=2 78 opt u' 0 ' 7. Critical Load Versus Rise Parameter for ^opt and V Bo= 10-0' n=2 78 8. Critical Load Versus Rise Parameter for i . and I , 3 = 0, n=2 79 opt u 0 9a. Anti-Symmetric Response, Different Designs, 3 = °°, n=2 80 0 9b. Anti-Symmetric Response, Different Designs, S =10, n=2 81 9c. Anti-Symmetric Response, Different Designs, 3 =0, n=2. . 82 o .9d. Limit Point Load Versus Rise Parameter for Symmetric Optimum Designs at e=6, 8, and 10, 3 =~, n=2. . 83 Q Vlll Figure Page 9e. Limit Point Load Versus Rise Parameter for Symmetric Optimum Designs at e=6, 8, and 10, 3 =0, n=2 . 83 o 10. Symmetric Critical Response, Symmetric Optimum Designs at e=6, 8, 10,3 =co, n=l,3 84 11. Variation in Symmetric Optimum Designs with Rise Parameter, 3 = °° n=2 85 0 12. Variation in Symnietric Optimum Designs with n, 3 =oo, e=10,0. 86 0 13. Variation in Symmetric Optimum Designs with Boundary Conditions, e=6, n=2 87 14. Critical Response of I , 1 ,, and-I 3 =«», n=2. I . . . . ?. ?P* . . ? ?^ 88 o 15. Critical Response of I , 1 , , and i . r J & =10,n=2. . . . . . ?. ?Pf . . .6.°?t 89 0 A S 16. Critical Response of I , I , , and _i B =0, n=2. . . . . . ? '. ?PV. . A0?* 90 o Al. Critical Load Vs. Rise Parameter, Simply Supported, Half Sine Load, Half Sine Arch 112 A2. Critical Load Vs. Rise Parameter, Clamped, Half Sine Load, Half Sine Arch 112 A3. Critical Load Vs. Rise Parameter, Simply Supported, Uniform Load, Parabolic Arch 113 A4. Effect of Rotational Restraint, Symmetric Response. 114 A5, Effect of Rotational Restraint, Anti-Symmetric Response, Half Sine Load, Half Sine Arch 114 A6. Critical Load Vs. Rise Parameter, Simply Supported, Uniform Load, Half Sine Arch 115 A7. Critical Load Vs, Rise Parameter, Clamped, Uniform Load, Half Sine Arch 115 CI. Comparison of Analytic and Finite Element Optimum Shapes, Anti-Symmetric Buckling, 3 =00, =2 " li9 n 0 ix Figure Page Dl. Relation Between Number of Iterations to Convergence and Starting Value of EXPl . . . 148 D2. Flow Chart for Anti-Symmetric Optimization . . . 151 D3. Flow Chart for Symmetric Optimization 152

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initial shape and load distribution, the one with the highest buckling load. This problem . shape, loading and boundary conditions). It will be shown This integro-differential equation relates the optimum shape. I. (£) to the primary
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