A Collection of Technical Papers: AIAA 77-182 - AIAA 77-242. (With omissions in numbering)
American Institute of Aeronautics and Astronautics, 1977 - Technology & Engineering
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Aeronautics and Astronautics AIAA airfoil analysis approximately argon axial blade row boattail boundary conditions boundary layer bubbles calculated cell coefficient combustion combustor conductivity configurations constant convection coolant cooling diameter diffusion flames displacement thickness downstream droplet effect energy entrainment equation exit experimental experiments finite flame speed flow field fluctuations fluid freestream fuel geometry gradient grid heat pipe heat transfer increase injection Institute of Aeronautics interaction inviscid iteration laser liquid Mach number maximum measured metal foam method mixer mixing NASA nozzle obtained parameter particle plane plume predicted present pressure distribution probe profiles Q-switch radial ratio region Reynolds number rotor sample scale separation shock wave shown in Figure solution space specimen stagnation pressure stator stream strong interaction subsonic supersonic surface technique temperature thermal thermocouple tion Transonic Flow tube tungsten turbulent values velocity viscous wall wing yaw angle