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Analytical study of aerodynamic means of controlling supersonic inlet flow, part I Technical report no. 495BMeans for achieving variable geometry supersonic inlet without using mechanical devices
Document ID
19660030698
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rosenbaum, H. (General Applied Science Labs., Inc. Westbury, NY, United States)
Zeiberg, S. L. (General Applied Science Labs., Inc. Westbury, NY, United States)
Date Acquired
August 3, 2013
Publication Date
November 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-66209
Report Number: NASA-CR-66209
Accession Number
66N39988
Funding Number(s)
CONTRACT_GRANT: NAS1-4387
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INLET FLOW
SUPERSONIC FLOW
VARIABLE GEOMETRY STRUCTURE

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