3-dimensional analysis of supersonic contoured nozzles; study undertaken in order to arrive at design of short, axially symmetric nozzles having axially directed exhaust and either, or both, improved performance and less weight than conventional conical nozzles; procedure for applying characteristic method of flow analysis in nozzle in arriving at proper nozzle wall contour for axial exhaust.
Philosophy for improved rocket nozzle design
Jet Propulsion
Jet Propulsion ; 27 , n 10
1957
6 pages
Article (Journal)
English
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