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Appendix approximate solutions atoms average duty cycle axial singularity distribution axis basic body Bodies of Revolution boundary conditions burst duration cambered body central body ceramics cold wall complete ring constant cosada Douglas Aircraft Company drag-due-to-lift correlation ellipse equation Fourier components Fourier series fuselage half the wetted half-ring wing heat transfer histogram interval lift distribution load distribution melting point minimum vortex drag modulus non-catalytic normalized duty cycle optimum overdense oxygen paper parameter planar-rectangular PR PR PR2K PROJECT RAND recombination recommendations expressed reference area reflect the official Region Research Memorandum ring-body configuration Sears-Haack body semi-minor axis skin friction softening temperature Supersonic surface reaction rates thermal conduction tion total burst TT-arc U.S. AIR FORCE underdense trails upper vhere views or policies volume reaction rates vortex drag-due-to-lift wail wave drag wave drag-due-to-lift wetted area zero