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Determination of the Stability and Control Characteristics of a Straight-Wing, Tailless Fighter-Airplane Model in the Langley Free-Flight Tunnel
Document ID
19930092559
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ankenbruck, Herman O
Date Acquired
August 15, 2013
Publication Date
February 1, 1946
Report/Patent Number
NACA-WR-L-199
NACA-ACR-L5K05
Report Number: NACA-WR-L-199
Report Number: NACA-ACR-L5K05
Accession Number
93R21849
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CENTER OF GRAVITY - POSITION
AIRPLANES - NACA (AMER )
PROPELLERS, PUSHER
AIRPLANES, TAILLESS
STABILITY & CONTROL
GENESE 35
PROPELLERS - WINDMILLING
AIRPLANES - TRIM
WIND TUNNEL TESTS - NACA - FREE-SPINNING (15') (LMAL)
AIRFOILS - RHODE ST
AIRPLANES, FIGHTER

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