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Flow field for an underexpanded, supersonic nozzle exhausting into an expansive launch tubeStatic pressure distributions along the launcher wall and pitot pressure measurements from the annular region between the rocket and the launcher were made as an underexpanded supersonic nozzle exhausted into an expansive launch tube. The flow remained supersonic along the entire length of the launcher for all nozzle locations studied.
Document ID
19770003433
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Morris, R. R. (Texas Univ. Austin, TX, United States)
Bertin, J. J. (Texas Univ. Austin, TX, United States)
Batson, J. L. (Texas Univ. Austin, TX, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: NASA. Langley Res. Center Advan. in Eng. Sci., Vol. 4
Subject Category
Spacecraft Propulsion And Power
Accession Number
77N10375
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19770003403Collected WorksAdvances in Engineering Science, Volume 4
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