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Comparison of flight and wind tunnel measurements of jet noise for the XV-5B aircraftWind tunnel tests to determine noise data from scale model research aircraft are discussed. Comparisons are made between data obtained in wind tunnels and results of full scale flight tests. The acoustic measurements for the XV-5B V/STOL fan research aircraft are presented.
Document ID
19730001302
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Atencio, A., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Kirk, J. V. (NASA Ames Research Center Moffett Field, CA, United States)
Soderman, P. T. (NASA Ames Research Center Moffett Field, CA, United States)
Hall, L. P. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-62182
Report Number: NASA-TM-X-62182
Accession Number
73N10029
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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