A model for 3-D sonic/supersonic transverse fuel injection into a supersonic air streamA 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.
Document ID
19890038005
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bussing, Thomas R. A. (Boeing Advanced Systems Co. Seattle, WA, United States)
Lidstone, Gary L. (Boeing Advanced Systems Seattle, WA, United States)