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V/STOL tilt rotor study. Volume 6: Hover, low speed and conversion tests of a tilt rotor aeroelastic model (Model 300)Stability and control tests of a scale model of a tilt rotor research aircraft were conducted. The characteristics of the model for hover, low speed, and conversion flight were analyzed. Hover tests were conducted in a rotor whirl cage. Helicopter and conversion tests were conducted in a low speed wind tunnel. Data obtained from the tests are presented as tables and graphs. Diagrams and illustrations of the test equipment are provided.
Document ID
19730022218
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Marr, R. L. (Bell Helicopter Co. Fort Worth, TX, United States)
Sambell, K. W. (Bell Helicopter Co. Fort Worth, TX, United States)
Neal, G. T. (Bell Helicopter Co. Fort Worth, TX, United States)
Date Acquired
September 2, 2013
Publication Date
May 15, 1973
Subject Category
Aircraft
Report/Patent Number
BELL-301-099-002-VOL-6
NASA-CR-114615
Report Number: BELL-301-099-002-VOL-6
Report Number: NASA-CR-114615
Accession Number
73N30950
Funding Number(s)
CONTRACT_GRANT: NAS2-6599
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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