Numerical Study of Mach 6 Boundary Layer Stabilization by Means of a Porous Surface
Sandham, N.D. and Lüdeke, H. (2009) Numerical Study of Mach 6 Boundary Layer Stabilization by Means of a Porous Surface. AIAA Journal, Vol. 47 (No. 9), pp. 2243-2252.
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Abstract
Direct numerical simulations are carried out of 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 modelled, 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.
| Document Type: | Article | ||||||
|---|---|---|---|---|---|---|---|
| Title: | Numerical Study of Mach 6 Boundary Layer Stabilization by Means of a Porous Surface | ||||||
| Authors: |
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| Date: | September 2009 | ||||||
| Journal or Publication Title: | AIAA Journal | ||||||
| Refereed publication: | Yes | ||||||
| In Open Access: | No | ||||||
| In SCOPUS: | Yes | ||||||
| In ISI Web of Science: | Yes | ||||||
| Volume: | Vol. 47 | ||||||
| Page Range: | pp. 2243-2252 | ||||||
| Status: | Published | ||||||
| Keywords: | Transition control, porous surface, hypersonic, direct numerical simulation | ||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||
| HGF - Program: | Space | ||||||
| HGF - Program Themes: | W RP - Raumtransport | ||||||
| DLR - Research area: | Space | ||||||
| DLR - Program: | W RP - Raumtransport | ||||||
| DLR - Research theme (Project): | W - Projekt IMENS-3C (old) | ||||||
| Location: | Braunschweig | ||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Spacecraft | ||||||
| Deposited By: | Dr.-Ing. Heinrich Lüdeke | ||||||
| Deposited On: | 15 Feb 2010 13:36 | ||||||
| Last Modified: | 13 Feb 2013 15:00 |
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