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. At the conditions studied, the numerical results show that combustion in the scramjet is mainly mixing limited.
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Brescianini et al. (1993) studied this question.
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