NASA NTRS · 19810014654
An analytical procedure and automated computer code used to design model nozzles which meet MSFC base pressure similarity parameter criteria
Abstract
Fundamental equations and similarity definition and application are described as well as the computational steps of a computer program developed to design model nozzles for wind tunnel tests conducted to define power-on aerodynamic characteristics of the space shuttle over a range of ascent trajectory conditions. The computer code capabilities, a user's guide for the model nozzle design program, and the output format are examined. A program listing is included.
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Sulyma, P. R.. 1980-05-01. An analytical procedure and automated computer code used to design model nozzles which meet MSFC base pressure similarity parameter criteria. https://ntrs.nasa.gov/citations/19810014654
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