The present use of a parabolized Navier-Stokes solver to accurately simulate the flowfield in a supersonic inlet yields good agreement between numerical analysis and experiment for a Mach 7.4 inlet under cruise conditions, with an internal compression ratio of 8. The significance of real gas effects on the performance calculation of a hypersonic inlet is demonstrated, with small changes in the ratio of specific heats resulting in a substantial change in the calculated pitot pressure ratio.
Real gas effects on the numerical simulation of a hypersonic inlet
1986-08-01
Sonstige
Keine Angabe
Englisch
Numerical Simulation of Hypersonic Inlet Flows
British Library Conference Proceedings | 1998
|Numerical Simulation of Hypersonic Inlet Flows
British Library Conference Proceedings | 1998
|Numerical simulation of hypersonic inlet flows
AIAA | 1998
|Numerical Simulation of Gaseous Hydrocarbon Fuel Injection in a Hypersonic Inlet
Online Contents | 2010
|