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Evaluation of the tilt rotor concept: The XV-15's roleThe need for an aircraft combining the efficient vertical takeoff and landing capability of a helicopter with the efficient high speed characteristics of a fixed wing turboprop is examined. The ability of the tilt rotor concept to fill this requirement and examples as to its potential usefulness in both military and civil missions is discussed.
Document ID
19780011199
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brown, J. H., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Edenborough, H. K. (Textron Bell Helicopter Fort Worth, Tex., United States)
Wernicke, K. G. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: AGARD Rotorcraft Design
Subject Category
Aircraft Design, Testing And Performance
Accession Number
78N19142
Distribution Limits
Public
Copyright
Other
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