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Subliming Layers Would Reveal Aerodynamic EffectsIn proposed technique, flow of fluid across surface studied in detail by use of multilayered, multicolored coating. Particularly useful in study of flow of air over small area of aerodynamic surface. By use of this method, incremental determinations made as to friction, transfer of heat, positions of shock waves, and position and extent of turbulence on given surface. Technique applied to surface of model in wind tunnel or to aerodynamics surface on aircraft.
Document ID
19890000602
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Jensen, Ronald N.
(NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 14, 2013
Publication Date
December 1, 1989
Publication Information
Publication: NASA Tech Briefs
Volume: 13
Issue: 12
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
LAR-13742
Report Number: LAR-13742
ISSN: 0145-319X
Accession Number
89B10602
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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