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Stability and control of compressible flows over a surface with concave-conves curvatureThe active control of spatially unstable disturbances in a laminar, two-dimensional, compressible boundary layer over a curved surface is numerically simulated. The control is effected by localized time-periodic surface heating. We consider two similar surfaces of different heights with concave-convex curvature. In one, the height is sufficiently large so that the favorable pressure gradient is sufficient to stabilize a particular disturbance. In the other case the pressure gradient induced by the curvature is destabilizing. It is shown that by using active control that the disturbance can be stabilized. The results demonstrate that the curvature induced mean pressure gradient significantly enhances the receptivity of the flow localized time-periodic surface heating and that this is a potentially viable mechanism in air.
Document ID
19860020303
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Maestrello, L.
(NASA Langley Research Center Hampton, VA, United States)
Bayliss, A.
(NASA Langley Research Center Hampton, VA, United States)
Parikh, P.
(NASA Langley Research Center Hampton, VA, United States)
Turkel, E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:178143
NASA-CR-178143
ICASE-86-48
Report Number: NAS 1.26:178143
Report Number: NASA-CR-178143
Report Number: ICASE-86-48
Accession Number
86N29775
Funding Number(s)
CONTRACT_GRANT: NAS1-17919
CONTRACT_GRANT: NAS1-17070
PROJECT: RTOP 505-31-83-01
CONTRACT_GRANT: NAS1-18107
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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