A computer program for modelling 2D hypersonic flows of gases containing water vapor and liquid water droplets is presented. The effects of interphase mass, momentum and energy transfer are studied. Computations are compared with existing quasi-1D calculations on the nozzle of the NASA Langley Eight Foot High Temperature Tunnel, a hypersonic wind tunnel driven by combustion of natural gas in oxygen enriched air.
Computation of hypersonic flows with finite rate condensation and evaporation of water
AIAA, Aerospace Sciences Meeting and Exhibit ; 1993 ; Reno, NV, United States
01.01.1993
Aufsatz (Konferenz)
Keine Angabe
Englisch
Computation of Hypersonic Flows With Finite-Catalytic Walls
British Library Conference Proceedings | 1994
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