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Approximate method for predicting form and location of detached shock waves ahead of plane or axially symmetric bodies
Document ID
19930082597
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Moeckel, W E
Date Acquired
August 16, 2013
Publication Date
July 1, 1949
Report/Patent Number
NACA-TN-1921
Report Number: NACA-TN-1921
Accession Number
93R11887
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW - DUCTS
FLOW - BODIES
AIR FLOW - ENGINE COWLINGS
FLOW - SHOCK WAVES
BODIES - DRAG
INLETS
THEORIES - FLOW
SUPERSONIC

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