Propulsive performance of hypersonic oblique detonation wave and shock-induced combustion ramjets

Journal of Propulsion and Power

Volumn 17, Issue 3, 2001, Pages 599-604

  Sislian, J P ^a   Schirmer, H ^a   Dudebout, R ^a   Schumacher, J ^a  

^a UNIVERSITY OF TORONTO   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTORS; COMPUTER SIMULATION; HYDROGEN; HYPERSONIC FLOW; SHOCK WAVES;

COMBUSTION RAMJETS; EULER EQUATIONS;

JETS;

EID: 0035332217     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5783     Document Type: Article

References (16)

1. Numerical simulation of hypersonic shock-induced combustion ramjets
2. A preliminary study of the application of steady-state detonation combustion to a reaction engine
3. Oblique detonation wave ramjet
4. Standing oblique detonation wave engine performance
5. Oblique detonation wave engine performance prediction
6. Aerodynamic and propulsive performance of hypersonic detonation wave ramjets
7. Hypersonic shock-induced combustion ramjet performance analysis
8. A lower-upper symmetric Gauss-Seidel method for the Euler and Navier-Stokes equations
9. Experiments on shock-induced combustion
10. Incomplete fuel/air mixing and off-design flight effects on hypersonic shock-induced combustion ramjet performance