Boundary conditions prove critical. Conference paper describes algorithm for calculation of shocks in hypersonic flows of gases at chemical equilibrium. Although algorithm represents intermediate stage in development of reliable, accurate computer code for two-dimensional flow, research leading up to it contributes to understanding of what is needed to complete task.
Calculating Shocks In Flows At Chemical Equilibrium
NASA Tech Briefs ; 12 , 9
1988-10-01
Miscellaneous
No indication
English
Calculating Shocks In Chemically Reacting Flows
NTRS | 1992
|Axisymmetric internal flows with shocks
AIAA | 1979
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