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In-flight measurement of rotor hub drag using the RSRA - A feasibility demonstrationThe Rotor Systems Research Aircraft (RSRA) is a compound helicopter that was test flown as a fixed-wing aircraft, with the main rotor blades removed and the rotor hub installed. An onboard rotor load-measurement system measured the resulting rotor hub drag and lift. Measured hub drag and lift are plotted for comparison to that predicted by full-scale and 1/6-scale model wind-tunnel tests. The success of the demonstration gives confidence that planned improvements to the RSRA will allow high-accuracy hub drag and lift measurements to be made in flight on a routine research basis.
Document ID
19870061693
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Acree, C. W., Jr.
(NASA Ames Research Center Moffett Field, CA, United States)
Kufeld, Robert M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
September 1, 1985
Subject Category
Aircraft Design, Testing And Performance
Accession Number
87A48967
Distribution Limits
Public
Copyright
Other

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