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Preliminary report on in-flight measurement of rotor hub drag and lift using the RSRAThe 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
19860003851
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Acree, C. W., Jr.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
REPT-85288
NASA-TM-86764
NAS 1.15:86764
Report Number: REPT-85288
Report Number: NASA-TM-86764
Report Number: NAS 1.15:86764
Accession Number
86N13319
Funding Number(s)
PROJECT: RTOP 505-42-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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