A model for sonic/supersonic transverse fuel injection into a supersonic airstream is proposed. The model replaces the hydrogen jet up to the Mach disk plane and the elliptic parts of the air flow field around the jet by an equivalent body. The main features of the model were validated on the basis of experimental data.
A model for 3-D sonic/supersonic transverse fuel injection into a supersonic air stream
1989-01-01
Conference paper
No indication
English
CONTROL OF A TRANSVERSE SUPERSONIC JET INJECTION INTO A SUPERSONIC CROSS-STREAM
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