A wall-injected, hydrogen-fueled scramjet is modeled numerically using a parabolic Navier-Stokes computer code with a k-epsilon turbulence model and finite-rate chemistry. The numerical results are compared to experimental scramjet data taken in a shock tunnel and are found to be in reasonable agreement. Under the conditions studied, the numerical results show that combustion in the scramjet is mainly mixing limited.
Numerical modeling of wall-injected scramjet experiments
Journal of Propulsion and Power ; 9 , 2
1993-04-01
Miscellaneous
No indication
English
Numerical modeling of wall-injected scramjet experiments
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