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A second order slender wing theory for wings with leading edge separation in supersonic flowSecond order slender wing theory for calculating supersonic flow over low aspect ratio wings with subsonic leading edges and leading edge separation
Document ID
19710024528
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nenni, J. P. (State Univ. of New York Buffalo, NY, United States)
Tung, C. (State Univ. of New York Buffalo, NY, United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1971
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-1860
AF-2883-S-1
Report Number: NASA-CR-1860
Report Number: AF-2883-S-1
Accession Number
71N34004
Funding Number(s)
CONTRACT_GRANT: NAS1-9543
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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