Title: The flow of a jet from a body opposing a supersonic free stream
Abstract: A series of experiments is described in which a jet issues from an orifice at the nose of a body in supersonic flow to oppose the mainstream. An analytical model of the flow is developed which suggests that the aerodynamic features of a steady flow depend primarily on a jet flow-force coefficient, and the Mach number of the jet in its exit plane. A sufficient condition for steady flow is developed. The experiments are found to agree well with predictions based on the flow model. A short account is presented of some previous investigations, and some of their conclusions are re-examined in the light of the present study.
Publication Year: 1966
Publication Date: 1966-10-01
Language: en
Type: article
Indexed In: ['crossref']
Access and Citation
Cited By Count: 263
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