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Flow of a compressible fluid past a symmetrical airfoil in a wind tunnel and in free air
Document ID
19930082372
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Emmons, Howard W (Harvard University)
Date Acquired
August 16, 2013
Publication Date
November 1, 1948
Report/Patent Number
NACA-TN-1746
Report Number: NACA-TN-1746
Accession Number
93R11662
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW MEASUREMENT - RELAXATION METHOD
FLOW - SHOCK WAVES
FLOW - AIRFOILS, SYMMETRICAL
PRESSURE DISTRIBUTION - AIRFOILS - NACA 0012
FLOW - SHOCK WAVES
AIRFOILS - NACA 0012 - ORDINATES
EFFECT OF COMPRESSIBILITY

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