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A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layerMathematical model for determining total drag of pointed body of revolution in supersonic flow with turbulent boundary layer
Document ID
19690010571
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Jackson, C. M., Jr. (NASA Langley Research Center Hampton, VA, United States)
Smith, R. S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5046
Report Number: NASA-TN-D-5046
Accession Number
69N19925
Funding Number(s)
CONTRACT_GRANT: 722-01-00-02-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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