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User's guide and description of the streamline divergence computer programThe streamline divergence program was developed to demonstrate the capability to trace inviscid surface streamlines and to calculate outflow-corrected laminar and turbulent convective heating rates on surfaces subjected to exhaust plume impingement. The analytical techniques used in formulating this program are discussed. A brief description of the streamline divergence program is given along with a user's guide. The program input and output for a sample case are also presented.
Document ID
19750011519
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sulyma, P. R.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Mcanally, J. V.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
LMSC-HREC-TM-D390450
NASA-CR-141717
Report Number: LMSC-HREC-TM-D390450
Report Number: NASA-CR-141717
Accession Number
75N19591
Funding Number(s)
CONTRACT_GRANT: NAS9-13429
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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