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An innovative technique for static and dynamic V/STOL testingInitial hover testing of the Navy's XFV-12A V/STOL technology prototype aircraft is being conducted in the former Lunar Lander Research Facility at the NASA Langley Research Center. The aircraft incorporates a unique lift/control concept for V/STOL flight. A key element in the development of this aircraft has been the application of existing hardware and facilities to conserve program funds. Adaptation of the NASA Gantry has created a V/STOL aircraft test facility with unique capability and flexibility. Static lift and control measurements can be obtained and dynamic hover flight can be conducted over a wide range of realistic test conditions.
Document ID
19790034152
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Lewis, E. L.
(U.S. Navy, Naval Air Systems Command, Washington D.C., United States)
Culpepper, R. G.
(NASA Langley Research Center Hampton, Va., United States)
Hancock, V. R.
(Rockwell International Corp. Columbus Aircraft Div., Columbus, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AHS 78-42
Report Number: AHS 78-42
Meeting Information
Meeting: In: American Helicopter Society, Annual National Forum
Location: Washington, DC
Start Date: May 15, 1978
End Date: May 17, 1978
Accession Number
79A18165
Distribution Limits
Public
Copyright
Other

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