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Prediction techniques for jet-induced effects in hover on STOVL aircraftPrediction techniques for jet induced lift effects during hover are available, relatively easy to use, and produce adequate results for preliminary design work. Although deficiencies of the current method were found, it is still currently the best way to estimate jet induced lift effects short of using computational fluid dynamics. Its use is summarized. The new summarized method, represents the first step toward the use of surface pressure data in an empirical method, as opposed to just balance data in the current method, for calculating jet induced effects. Although the new method is currently limited to flat plate configurations having two circular jets of equal thrust, it has the potential of more accurately predicting jet induced effects including a means for estimating the pitching moment in hover. As this method was developed from a very limited amount of data, broader applications of the method require the inclusion of new data on additional configurations. However, within this small data base, the new method does a better job in predicting jet induced effects in hover than the current method.
Document ID
19910022756
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Wardwell, Douglas A.
(NASA Ames Research Center Moffett Field, CA., United States)
Kuhn, Richard E.
(Kuhn, Richard E., San Diego CA , United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.15:102818
NASA-TM-102818
A-90146
Report Number: NAS 1.15:102818
Report Number: NASA-TM-102818
Report Number: A-90146
Accession Number
91N32070
Funding Number(s)
PROJECT: RTOP 505-68-71
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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