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Investigation of normal shock inlets for highly maneuverable aircraftConcepts are investigated for obtaining both low cowl drag and good inlet performance at high angles of attack. The effect of a canard on inlet performance for a kidney shaped inlet in each of two vertical locations is discussed along with a sharp lip two dimensional inlet on a canardless forebody.
Document ID
19770008083
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Martin, A. W. (Rockwell International Corp. Los Angeles, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1977
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-137970
Report Number: NASA-CR-137970
Accession Number
77N15026
Funding Number(s)
CONTRACT_GRANT: NAS2-8955
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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