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Charts of additive drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attackCharts of additive drag coefficient and mass flow ratio for inlets utilizing right circular cones at zero angle of attack
Document ID
19660016261
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
May 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3434
Report Number: NASA-TN-D-3434
Accession Number
66N25550
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CHART
CONICAL INLET
DRAG COEFFICIENT
MASS FLOW

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