The Oblique Detonation Wave Engine (ODWE) for hypersonic flight has been analytically studied by NASA using the CFD codes which fully couple finite rate chemistry with fluid dynamics. Fuel injector designs investigated included wall and strut injectors, and the in-stream strut injectors were chosen to provide good mixing with minimal stagnation pressure losses. Plans for experimentally validating the ODWE concept in an arc-jet hypersonic wind tunnel are discussed. Measurements of the flow field properties behind the oblique wave will be compared to analytical predictions.
Analytical and experimental validation of the Oblique Detonation Wave Engine concept
1988-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Oblique Detonation Wave Engine Performance Prediction
Online Contents | 1996
|Oblique detonation wave engine performance prediction
AIAA | 1995
|Standing oblique detonation wave engine performance
AIAA | 1987
|Oblique detonation wave engine performance prediction
AIAA | 1996
|