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Analysis and design of three dimensional supersonic nozzles. Volume 3: A design technique for multiple nozzle configurationsAn iteration procedure for optimum nozzle design with application to hypersonic aircraft is discussed. In the procedure, intial values of several of the design parameters are assumed from simplified approximate considerations and are then varied systematically in order to determine the value of each parameter which optimizes nozzle performance. Improvements in nozzle performance are obtained by perturbing the initially assumed values of the geometric parameters on the basis of a computer analysis.
Document ID
19740003002
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ferri, A. (Advanced Technology Labs., Inc. Westbury, NY, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
ATL-TR-166-VOL-3
NASA-CR-132352
Report Number: ATL-TR-166-VOL-3
Report Number: NASA-CR-132352
Accession Number
74N11115
Funding Number(s)
CONTRACT_GRANT: NAS1-10327
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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