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Tests of a Full-Scale Model of the Republic XF-91 Airplane in the Ames 40- by 80-Foot Wind Tunnel. Force and Moment DataWind-tunnel tests of a full-scale model of the Republic XF-91 airplane having swept-back wings and a vee tail were conducted to determine both the stability and control characteristics of the model longitudinally, laterally, and directionally. Configurations of the model were investigated involving such variables as external fuel tanks, a landing gear, trailing-edge flaps, leading-edge slats, and a range of wing incidences and tail incidences.
Document ID
20090026981
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Hunten, Lynn W. (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Dew, Joseph K. (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
August 24, 2013
Publication Date
May 4, 1949
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NACA-RM-SA9C04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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