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Preliminary results of boundary layer noise measured on the X-15 airplane.Boundary layer noise and effects of acoustic energy on panel response, panel fatigue and internal sound levels tested with X-15 aircraft
Document ID
19660030836
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kordes, E. E.
Tanner, C. S.
Date Acquired
August 3, 2013
Publication Date
January 1, 1965
Subject Category
Aircraft
Accession Number
66A10126
Distribution Limits
Public
Copyright
Other
Keywords
BOUNDARY LAYER NOISE
AERODYNAMIC NOISE
ACOUSTIC FATIGUE
X-15 AIRCRAFT

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