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Microphone Detects Waves In Laminar Boundary-Layer FlowSimple noninvasive acoustical technique effective in measurement of instability waves, which precede onset of turbulence in laminar boundary layer flows. Microphone mounted below surface detects pressure waves indicative of instabilities in laminar flow. Relatively insensitive to long-wavelength background noise. Such measurements important in research on aerodynamic flows and potential applications in control of turbulence (with consequent reduction of drag) on aircraft.
Document ID
19900000582
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kendall, James M.
(Caltech)
Date Acquired
August 14, 2013
Publication Date
November 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 11
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
NPO-17479
Report Number: NPO-17479
ISSN: 0145-319X
Accession Number
90B10582
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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