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Correlation of low speed wind tunnel and flight test data for V/STOL aircraftThe XV-5B fan-in-wing aircraft and the Y0V-10 RCF rotating cylinder flap aircraft were subjected to wind tunnel tests. These tests were conducted specifically to provide for correlation between wind tunnel and inflight aerodynamics and noise test data. Correlation between aerodynamic and noise data are presented and testing techniques that are related to the accuracy of the data, or that might affect the correlations, are discussed.
Document ID
19750015485
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Cook, W. L. (NASA Ames Research Center Moffett Field, CA, United States)
Hickey, D. H. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-X-62423
A-5998
Report Number: NASA-TM-X-62423
Report Number: A-5998
Accession Number
75N23557
Funding Number(s)
PROJECT: RTOP 514-54
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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