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Wind tunnel and flight test of the XV-15 Tilt Rotor Research AircraftThe XV-15 Tilt Rotor Research Aircraft Project involves design, fabrication, and flight testing of two aircraft. This program is currently in the test phase for concept evaluation and substantiation of design. As part of this evaluation, one of the aircraft was tested in the NASA-Ames 40- by 80-foot wind tunnel. The status of testing to date and some of the results of the wind tunnel and flight tests are presented.
Document ID
19790065092
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Marr, R. L. (Textron Bell Helicopter Fort Worth, TX, United States)
Blackman, S. (Bell Helicopter Textron Fort Worth, Tex., United States)
Weiberg, J. A. (NASA Ames Research Center Moffett Field, Calif., United States)
Schroers, L. G. (U.S. Army, Aeromechanics Laboratory, Moffett Field Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AHS 79-54
Meeting Information
Meeting: American Helicopter Society, Annual National Forum
Location: Washington, DC
Start Date: May 21, 1979
End Date: May 23, 1979
Sponsors: American Helicopter Society
Accession Number
79A49105
Distribution Limits
Public
Copyright
Other

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