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Rotor systems research aircraft simulation mathematical modelAn analytical model developed for evaluating and verifying advanced rotor concepts is discussed. The model was used during in both open loop and real time man-in-the-loop simulation during the rotor systems research aircraft design. Future applications include: pilot training, preflight of test programs, and the evaluation of promising concepts before their implementation on the flight vehicle.
Document ID
19780005098
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Houck, J. A.
(NASA Langley Research Center Hampton, VA, United States)
Moore, F. L.
(NASA Langley Research Center Hampton, VA, United States)
Howlett, J. J.
(Sikorsky Aircraft Hampton, VA, United States)
Pollock, K. S.
(NASA Langley Research Center Hampton, VA, United States)
Browne, M. M.
(NASA Langley Research Center)
Date Acquired
September 3, 2013
Publication Date
November 1, 1977
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-78629
Report Number: NASA-TM-78629
Accession Number
78N13041
Funding Number(s)
PROJECT: RTOP 745-01-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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