A Collection of Technical Papers: AIAA Fifth Annual Structures and Materials Conference, Palm Springs, California, Riviera Hotel, April 1-3, 1964
American Institute of Aeronautics and Astronautics, 1964 - Composite materials - 479 pages
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ablator aerodynamic alloys aluminum analysis applied approximately axial bending booster boundary coefficient components compression configuration constant crack creep strain criteria cryopump curves cylinder deformation density determined diameter Douglas Aircraft Company dynamic effect elastic elastomer equation evaluation experimental factor of safety fatigue damage fiber metal filaments FINENESS RATIO flight flow flutter foam frequency function heat honeycomb hypervelocity impact increase insulation launch linear load cycles Mach number mass fraction material meteoroid method mission mode mode shapes modulus NASA obtained panels parameter payload penetration plastic pressure problem projectile propellant pyrolytic graphite range ratio residual stresses Reynolds number sandwich shear sheet shell shown in Figure simulation skin solution space steady stress stiffness stress concentrations structural weight surface tank target tensile theory thermal conductivity thermal stresses thickness tion titanium unsteady values variables vehicle velocity vibration zero