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The Effect of Mach Number on the Aerodynamic Characteristics of a Single-Engine Pursuit Airplane as Determined from Tests of a 1/3-Scale Model
Document ID
19930092693
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jessen, Henry
Date Acquired
September 6, 2013
Publication Date
May 3, 1945
Report/Patent Number
NACA-MR-A5E03
NACA-WR-A-76
Report Number: NACA-MR-A5E03
Report Number: NACA-WR-A-76
Accession Number
93R21983
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
RADIATORS, DUCT - VANES, DEFLECTOR
TAIL SURFACES - NORTH AMERICAN P-51
AIRPLANES - NORTH AMERICAN P-51 (EXPERIMENTAL)
WIND TUNNEL TESTS(AAL-HIGH-SPEED-16')(AMER )
WIND TUNNEL TESTS - AAL - HIGH-SPEED (16')
WIND TUNNEL TESTS(AAL-HIGH-SPEED-16')
MACH NUMBER
ELEVATORS - DEFLECTION
WING FLAPS, DIVE-CONTROL
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