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Langley Full-scale Tunnel Investigation of the Factors Affecting the Directional Stability and Trim Characteristics of a Fighter-Type
Document ID
19930092687
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lange, Roy H
Date Acquired
September 6, 2013
Publication Date
November 1, 1945
Report/Patent Number
NACA-WR-L-109
NACA-ARR-L5H09
Report Number: NACA-WR-L-109
Report Number: NACA-ARR-L5H09
Accession Number
93R21977
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES - GRUMMAN F6F-4 WIND TUNNEL TESTS (NACA-FULL-SCALE)(AMER)
TAIL SURFACES, VERTICAL - GRUMMAN F6F-4 WIND TUNNEL TESTS (NACA-
FUSELAGE-WING COMBINATIONS
STABILITY, DIRECTIONAL - GRUMMAN F6F-4
FULL-SCALE)
PROPELLER SLIPSTREAM - EFFECT ON STABILITY
AIRPLANES - TRIM
AIRPLANES, FIGHTER
AIR FLOW - MEASUREMENT

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