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Measurement Of Crossflow Vortex StructureMethod developed for measuring wavelengths of crossflow vortices by using surface-mounted, microthin, multielement hot-film sensors. Provides direct and true value of wavelength of crossflow vortices at various spanwise locations without localized flow disturbances. Attainment of laminar airflow on aircraft wings has significant potential for reducing drag and increasing fuel efficiency.
Document ID
19940000561
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Maddalon, Dal V. (NASA Langley Research Center, Hampton, VA.)
Agarwal, Navel K. (Analytical Services and Materials, Inc.)
Date Acquired
August 16, 2013
Publication Date
October 1, 1994
Publication Information
Publication: NASA Tech Briefs
Volume: 18
Issue: 10
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
LAR-14824
Accession Number
94B10561
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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