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Design of optimized three-dimensional thrust nozzle contoursDesign of optimized three-dimensional thrust nozzle contours
Document ID
19660014361
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Murthy, S. N. B. (Purdue Univ. West Lafayette, IN, United States)
Thompson, H. D. (Purdue Univ. West Lafayette, IN, United States)
Date Acquired
August 3, 2013
Publication Date
March 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
JPC-402
NASA-CR-74310
TM-65-2
Report Number: JPC-402
Report Number: NASA-CR-74310
Report Number: TM-65-2
Accession Number
66N23650
Funding Number(s)
CONTRACT_GRANT: NSG-592
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET NOZZLE
THREE-DIMENSIONAL FLOW
OPTIMIZATION

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