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Methodology for Three Dimensional Nozzle DesignCriteria for the selection and methods of analysis for designing a hypersonic scramjet nozzle are discussed. The criteria are based on external and internal flow requirements, related to drag, lift, and pitching moments of the vehicle and thrust of the engine. The steps involved in establishing the criteria are analyzed. Mathematical models of the design procedure are provided.
Document ID
19740014810
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ferri, A. (Advanced Technology Labs., Inc. Westbury, NY, United States)
Dash, S. (Advanced Technology Labs., Inc. Westbury, NY, United States)
Delguidice, P. (Advanced Technology Labs., Inc. Westbury, NY, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1974
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-132438
ATL-TR-195
Report Number: NASA-CR-132438
Report Number: ATL-TR-195
Accession Number
74N22923
Funding Number(s)
CONTRACT_GRANT: NAS1-12104
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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