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An Investigation of the McDonnell XP-85 Airplane in the Ames 40- by 80-Foot Wind Tunnel: Pressure-Distribution TestsPressure measurements were made during wind-tunnel tests of the McDonnell XP-85 parasite fighter. Static-pressure orifices were located over the fuselage nose, over the canopy, along the wing root, and along the upper and lower stabilizer roots. A total-pressure and static-pressure rake was located in the turbojet engine air-intake duct. It was installed at the station where the compressor face would be located. Pressure data were obtained for two airplane conditions, clean and with skyhook extended, through a range of angle of attack and a range of yaw.
Document ID
20050019260
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)
James, Harry A.
(National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
August 22, 2013
Publication Date
October 22, 1948
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-SA8J22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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