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Note on compressibility effects on downwash at the tail at subcritical speeds
Document ID
19930092476
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sweberg, Harold H
Date Acquired
September 6, 2013
Publication Date
March 1, 1945
Report/Patent Number
NACA-CB-L5C09
NACA-WR-L-19
Report Number: NACA-CB-L5C09
Report Number: NACA-WR-L-19
Accession Number
93R21766
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES - NORTH AMERICAN P-51B WIND TUNNEL TESTS (AMER )
LIFT COEFFICIENTS
AIRPLANES - LOCKHEED P-58 WIND TUNNEL TESTS (AMER )
LOAD DISTRIBUTION, WING-SPAN
TAIL SURFACES, HORIZONTAL
DOWNWASH ANGLES - EFFECT OF COMPRESSIBILITY

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