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Rotary-wing aircraft systems for the short-haul marketThis paper describes preliminary designs of tilt-rotor and tandem-rotor helicopter V/STOL aircraft for the 1958 short-haul market. These designs include a tilt-rotor aircraft designed for STOL-only operation. The baseline designs are presented with technological and cost data. The impact of noise and ride qualities on aircraft size and cost, and on passenger acceptance are discussed. The results of the study are compared against competitive alternatives in air transportation.
Document ID
19750038425
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Magee, J. P.
Clark, R. D. (Boeing Vertol Co. Philadelphia, Pa., United States)
Giulianetti, D. (NASA Headquarters Washington, DC United States)
Date Acquired
August 8, 2013
Publication Date
February 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 75-275
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Annual Meeting and Technical Display
Location: Washington, DC
Start Date: February 24, 1975
End Date: February 26, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A22497
Funding Number(s)
CONTRACT_GRANT: NAS2-8048
Distribution Limits
Public
Copyright
Other

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