AIAA 77-182 - AIAA 77-242. (With omissions in numbering)American Institute of Aeronautics and Astronautics, 1977 - Aeronautics |
Common terms and phrases
AIAA airfoil analysis approximation axial blade row boattail boundary conditions boundary layer calcium tartrate calculations cell coefficient combustion combustor configurations constant convection coolant cooling coordinate density diameter diffusion flames displacement thickness downstream droplet effect energy exit experimental experiments finite finite-difference flame speed flow field fluctuations fluid fuel geometry gradient grid points heat pipe heat transfer increase injection inlet Institute of Aeronautics interaction inviscid iterations laser liquid Mach number maximum measured mesh method mixing NASA nozzle obtained parameter particle perturbation plane plume predicted present pressure distribution probe profiles radial radial velocity ratio region relaxation Reynolds number rotor sample shock wave shown in Figure solution space stagnation pressure stream subsonic supersonic surface Swept Wings technique temperature thermal thermocouple three-dimensional tion trailing edge Transonic Flow tube turbulent upstream values velocity viscous wall wing