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wind-tunnel tests of the xv-15 tilt rotor aircraftThe XV-15 aircraft was tested in the Ames 40 by 80 Foot Wind Tunnel for preliminary evaluation of aerodynamic and aeroelastic characteristics prior to flight. The tests were undertaken to investigate the aircraft performance, stability, control and structural loads for flight modes from helicopter through transition and airplane mode up to the tunnel capability of 170 knots. Results from these tests are presented.
Document ID
19800015802
Document Type
Technical Memorandum (TM)
Authors
Weiberg, J. A. (NASA Ames Research Center Moffett Field, CA, United States)
Maisel, M. D. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1980
Subject Category
AIRCRAFT DESIGN, TESTING AND PERFORMANCE
Report/Patent Number
NASA-TM-81177
AVRADCOM-TR-80-A-3
A-8089
Funding Number(s)
PROJECT: RTOP 532-04-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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