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A method for determining the aerodynamic characteristics of two-and three-dimensional shapes at hypersonic speeds
Document ID
19930082281
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ivey, H Reese
Klunker, E Bernard
Bowen, Edward N
Date Acquired
August 16, 2013
Publication Date
July 1, 1948
Report/Patent Number
NACA-TN-1613
Report Number: NACA-TN-1613
Accession Number
93R11571
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW - BODIES, ROTATING
FLOW VELOCITY, HIGH - HYPERSONIC
LIFT COEFFICIENTS - AIRFOILS
THEORIES - FLOW
SUPERSONIC
PRESSURE COEFFICIENTS - AIRFOILS
PRESSURE DISTRIBUTION - BODIES
FLOW - SHOCK WAVES
PRESSURE DISTRIBUTION - AIRFOILS
LIFT - BODIES
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