Downloaded from https://www.everyspec.com $VflUCTIJRES IST OF ILLUSTRATIONS (WCmtised). Figure Title Page 3-1. Theoretical Deformations of Pressure Vessel under Membrane Stresses Alone-.... 42 3-2. Deforn-ations of Thin Circular Cylindrical Shell under Beriding Stresses 42 3-3. Determination Of Tangent Modulus and Secant Modu- lus from Stress-Stfain r 46 3-4. Bar Heated between Two Insulated Walls 47 3-5. Assumed Temperature Distribution in Long Rectan- gular Flat Plate 47 3-6. Ring Frame with Temperature 'Varying Linearly through Depth 48 3-7. Ring-Reinforced Circular Cylindrical Shell ----- 49 3-8. Simply Supported Plate Subjected to Thermal Stresses in One Direction .. . . . . 49 3-9.
Assumed Stress Distribution in Rectangular Flat Plate with Free Edges ... 50 3-10. Tensile Creep Curve ... 51 3-11. Deflected Column 53 3-12. Stress-Strain Curve at Elevated Temperature ... 54 4-1. Effects of Aerodynamic Heating on Model Nose Cone, Stagnation Temperature 1995OR ------- 59 4-2. Effects of Aerodynamic Heating on Model Nose Cone, Stagnation Temperature 2030'R -................ 59 4-4. Top Section, Redstone Missile ...................-.................. 65 -3, Tank Section, Jupiter Missile ....-.................-----------. 4 v