NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Numerical simulation of boundary layer excitation by surface heating/coolingThe concept of active control of growing disturbances in an unstable compressible flow by using time periodic, localized surface heating is studied numerically. The simulations are calculated by a fourth-order accurate solution of the compressible, laminar Navier-Stokes equations. Fourth-order accuracy is particularly important for this problem because the solution must be computed over many wavelengths. The numerical results demonstrate the growth of an initially small fluctuation into the nonlinear regime where a local breakdown into smaller scale disturbances can be observed. It is shown that periodic surface heating over a small strip can reduce the level of the fluctuation provided that the phase of the heating current is properly chosen.
Document ID
19850017445
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Bayliss, A.
(Exxon Corporate Research Sciences Labs. Hampton, VA, United States)
Maestrello, L.
(NASA Langley Research Center)
Parikh, P.
(Vigyan Research Associates, Inc.)
Turkel, E.
(Tel-Aviv Univ.)
Date Acquired
September 5, 2013
Publication Date
March 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ICASE-85-23
NASA-CR-172575
NAS 1.26:172575
Report Number: ICASE-85-23
Report Number: NASA-CR-172575
Report Number: NAS 1.26:172575
Accession Number
85N25756
Funding Number(s)
CONTRACT_GRANT: NAS1-17130
CONTRACT_GRANT: NAS1-16394
PROJECT: RTOP 505-31-83-01
CONTRACT_GRANT: NAS1-17070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available