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Discontinuous flows and free streamline solutions for axisymmetric bodies at zero and small angles of attackIntegral equations to calculate free streamline flow behind axisymmetric bodies at zero and small angles of attack
Document ID
19700012222
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Struck, H. G. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1970
Subject Category
Aerodynamics
Report/Patent Number
M160
NASA-TN-D-5634
Report Number: M160
Report Number: NASA-TN-D-5634
Accession Number
70N21527
Funding Number(s)
CONTRACT_GRANT: 933-50-07-00-62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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