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Calculated and Measured Turning Performance of a Navy F2A-3 Airplane as Affected by the Use of FlapsNo abstract available
Document ID
19930092640
Acquisition Source
Ames Research Center
Document Type
Other - NACA Wartime Report
Authors
Clousing, Lawrence A. (NASA Ames Research Center Moffett Field, CA, United States)
Gadeberg, Burnett L. (NASA Ames Research Center Moffett Field, CA, United States)
Kauffman, William M. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1943
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-WR-W-6
NACA-ACR-3I30
Accession Number
93R21930
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLYING, HIGH-ALTITUDE
WING FLAPS - DEFLECTION
AIRPLANES - BREWSTER F2A-3 FLIGHT TESTS (AMER )
AIRPLANES - WEIGHT
WING FLAPS, SPLIT - PARTIAL-SPAN
TURNING - BREWSTER F2A-3
WINGS - POLARS
LIFT COEFFICIENTS - BREWSTER F2A-3
PROPELLER THRUST

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