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Transpiration Control Of Aerodynamics Via Porous SurfacesQuasi-active porous surface used to control pressure loading on aerodynamic surface of aircraft or other vehicle, according to proposal. In transpiration control, one makes small additions of pressure and/or mass to cavity beneath surface of porous skin on aerodynamic surface, thereby affecting rate of transpiration through porous surface. Porous skin located on forebody or any other suitable aerodynamic surface, with cavity just below surface. Device based on concept extremely lightweight, mechanically simple, occupies little volume in vehicle, and extremely adaptable.
Document ID
19930000586
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Banks, Daniel W.
(NASA Langley Research Center, Hampton, VA.)
Wood, Richard M.
(NASA Langley Research Center, Hampton, VA.)
Bauer, Steven X. S.
(NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 16, 2013
Publication Date
September 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 9
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-14682
Accession Number
93B10586
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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