Computational Fluid Dynamics (CFD) has played a major role in the resurgence of hypersonic flight, on the premise that numerical methods will allow performance of simulations at conditions for which no ground test capability exists. Validation of CFD methods is being established using the experimental data base available, which is below Mach 8. It is important, however, to realize the limitations involved in the extrapolation process as well as the deficiencies that exist in numerical methods at the present time. Current features of CFD codes are examined for application to propulsion system components. The shortcomings in simulation and modeling are identified and discussed.
Advanced computational techniques for hypersonic propulsion
International Symposium on Air Breathing Engines ; 1989 ; Athens, Greece
1989-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Measurement techniques for hypersonic propulsion
NTRS | 1967
|NTRS | 1979
|NTRS | 1975
|