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Boundary layer blockage in expansion tube nozzlesThe results of a first order perfect gas correction for the effects of the boundary layer formation within expansion tubes with nozzles are presented. The analytical model developed to describe the boundary layer formation within the expansion tube and an expansion nozzle located at the end of the acceleration tube is based on the Karman integral equations. The results of this analytical model are compared with experimental data from an expansion diffuser. The model provides a useful tool for the preliminary design of nozzles for such facilities.
Document ID
19960001677
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sudnitsin, Olga
(Queensland Univ. Brisbane, Australia)
Morgan, Richard G.
(Queensland Univ. Brisbane, Australia)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: Shock Tunnel Studies of Scramjet Phenomena 1994
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
96N11685
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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