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An approximate solution of additive-drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attackIncompressible approximation solution of additive drag coefficient and mass flow ratio for inlets with right circular cones
Document ID
19700001663
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Mascitti, V. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5537
Report Number: NASA-TN-D-5537
Accession Number
70N10967
Funding Number(s)
CONTRACT_GRANT: 720-03-10-02-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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