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Forebody drag reductionIt is shown that the mechanisms of forebody drag reduction by means of either a spike or a forward-facing jet are similar, with the maximum achievable drag reduction being of the same order. Because the jet may be a relatively cool gas, however, the forward facing jet has the additional capability of reducing the aerodynamic heating that is so severe at high Mach numbers. By means of the correlation presented, jet ejection parameters may be chosen to achieve maximum permissible forebody drag reduction. The correlation method uses a momentum coefficient that characterizes jet efflux and freestream conditions.
Document ID
19810064683
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Pamadi, B. N.
(NASA Langley Research Center Hampton, VA; Indian Institute of Technology, Bombay, India)
Date Acquired
August 11, 2013
Publication Date
October 1, 1981
Publication Information
Publication: AIAA Journal
Volume: 19
Subject Category
Aerodynamics
Accession Number
81A49087
Distribution Limits
Public
Copyright
Other

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