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A rotor technology assessment of the advancing blade conceptA rotor technology assessment of the Advancing Blade Concept (ABC) was conducted in support of a preliminary design study. The analytical methodology modifications and inputs, the correlation, and the results of the assessment are documented. The primary emphasis was on the high-speed forward flight performance of the rotor. The correlation data base included both the wind tunnel and the flight test results. An advanced ABC rotor design was examined; the suitability of the ABC for a particular mission was not considered. The objective of this technology assessment was to provide estimates of the performance potential of an advanced ABC rotor designed for high speed forward flight.
Document ID
19830010441
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pleasants, W. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AVRADCOM-TR-82-A-18
A-9094
NAS 1.15:84298
NASA-TM-84298
Report Number: AVRADCOM-TR-82-A-18
Report Number: A-9094
Report Number: NAS 1.15:84298
Report Number: NASA-TM-84298
Accession Number
83N18712
Funding Number(s)
PROJECT: RTOP 532-06-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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