NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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
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
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

NameType 19730001302.pdf STI