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An Investigation of a Full-Scale Model of the Republic XF-91 Airplane in the Ames 40- By 80-Foot Wind Tunnel: Pressure DataWind-tunnel tests of a full-scale model of the Republic XF-91 airplane were conducted to determine the distribution of pressure over the external wing fuel tank installation and over the vee tail and ventral fin. The data were obtained for a range of angles of attack and sideslip and elerudder deflection angles; the presentation is in tabular form.
Document ID
20050019248
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Hunton, 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 22, 2013
Publication Date
March 25, 1949
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-RM-SA9C25
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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