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Conceptual design study of 1985 commercial tilt rotor transports. Volume 1: VTOL design summaryAircraft were synthesized in the 21-, 45-, and 100- passenger categories. Technological factors were considered and the 45-passenger point design, designated the D312, was selected. Variants of the D312 having sideline noise levels in hover of + or - 5 PNdB were also studied. All three 45-passenger aircraft were analyzed for performance, weights, economics, handling qualities, noise footprints, aeroelastic stability and ride comfort. Results are presented.
Document ID
19750013184
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Detore, J. A.
(Bell Helicopter Co. Fort Worth, TX, United States)
Sambell, K. W.
(Bell Helicopter Co. Fort Worth, TX, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1975
Publication Information
Publisher: NASA
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-CR-2544
D312-099-002-VOL-1
Report Number: NASA-CR-2544
Report Number: D312-099-002-VOL-1
Accession Number
75N21256
Funding Number(s)
CONTRACT_GRANT: NAS2-8259
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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