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Free-Flight-Tunnel Investigation of the Effect of the Fuselage Length and the Aspect Ratio and Size of the Vertical Tail on Lateral Stability and Control
Document ID
19930092574
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Draper, John W
Date Acquired
September 6, 2013
Publication Date
April 1, 1943
Report/Patent Number
NACA-WR-L-487
NACA-ARR-3D17
Report Number: NACA-WR-L-487
Report Number: NACA-ARR-3D17
Accession Number
93R21864
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY, DIRECTIONAL - REPUBLIC P-41
WIND TUNNEL BALANCES - NACA - FREE-FLIGHT
FINS & RUDDERS, TWIN - REPUBLIC P-41
TAIL SURFACES, VERTICAL - ASPECT RATIO
STABILITY TESTS - REPUBLIC P-41 WIND TUNNEL (NACA-FREE-FLIGHT)
PROPELLERS - WINDMILLING
STABILITY & CONTROL, LATERAL - REPUBLIC P-41
FUSELAGES - DESIGN
LIFT, DRAG & PITCHING MOMENTS - REPUBLIC P41

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