Welcome to e-Prints Soton!
Go to the home pageGo to you accountBrowse the archiveSearch e-Prints Soton
Numerical study of mach 6 boundary-layer stabilization by means of a porous surface

Sandham, Neil (2009) Numerical study of mach 6 boundary-layer stabilization by means of a porous surface. AIAA Journal, 47, (9), 2243-2252. (doi:10.2514/1.43388)
http://eprints.soton.ac.uk/69787/

Full text of this item is not available from this server.

Official URL: http://dx.doi.org/10.2514/1.43388

Abstract

Direct numerical simulations are carried out on boundary-layer flow at Mach 6 over a porous surface, in which a Mack mode of instability is excited. The pores are resolved rather than modeled, allowing an evaluation to be made of the accuracy of simplified analytical models used in previous investigations based on linear stability theory. It is shown that the stabilizing effect of porosity is stronger in the simulations than in the corresponding theory for both two- and three-dimensional pores. From comparisons of spanwise grooves, streamwise slots, and square pores, it appears that the detailed surface structure is not as important as the overall porosity, and the hydraulic diameter is able to collapse the results for different pore shapes to good accuracy. When the porous surface consists of fewer larger pores, the flow is noisier, with sound waves generated at the pore edges.

Item Type:Article
ID Code:69787
Date of issue:September 2009
ISSN:0001-1452
Subjects:Q Science > QA Mathematics
T Technology > TL Motor vehicles. Aeronautics. Astronautics
School or Centre:School of Engineering Sciences > Aerodynamics & Flight Mechanics
Deposited By:Sandham, Prof Neil
Deposited On:03 December 2009

Edit this item (Staff only)

References in Article

BRES GA
5 AIAA THEOR FLUID M 2008
2.
CARPENTER PW
Effects of passive porous walls on boundary-layer instability
AIAA JOURNAL 39 : 597 2001
3.
CHOKANI N
Nonlinear aspects of hypersonic boundary-layer stability on a porous surface
AIAA JOURNAL 43 : 149 2005
4.
EGOROV IV
2007948 AIAA 2007
5.
ENK S
NOTES NUMER IN PRESS :
6.
FEDOROV A
Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating
JOURNAL OF FLUID MECHANICS 479 : 99 DOI 10.1017/S0022112002003440 2003
7.
FEDOROV AV
Stabilization of hypersonic boundary layers by porous coatings
AIAA JOURNAL 39 : 605 2001
8.
GADELHAK M
FLOW CONTROL PASSIVE : 2007
9.
HERBERT T
Parabolized stability equations
ANNUAL REVIEW OF FLUID MECHANICS 29 : 245 1997
10.
KROLL N
8741 DFVLR FORSCH 1987
11.
LIEPMANN HW
ACTIVE CONTROL OF LAMINAR TURBULENT TRANSITION
JOURNAL OF FLUID MECHANICS 118 : 201 1982
12.
MACK LM
709 AGARD 1984
13.
MALIK MR
NUMERICAL-METHODS FOR HYPERSONIC BOUNDARY-LAYER STABILITY
JOURNAL OF COMPUTATIONAL PHYSICS 86 : 376 1990
14.
MASLOV AA
21722001 INT SCI TEC 2001
15.
RASHEED A
Experiments on passive hypervelocity boundary-layer control using an ultrasonically absorptive surface
AIAA JOURNAL 40 : 481 2002

©2003-2006 University of Southampton
Related Sites: University of Southampton, Library, TARDis Project, GNU EPrints Software.