Computational studies of the effect of wall temperature on hypersonic shock-induced boundary layer separation

Brown, L., Fischer, C., Boyce, R. R., Reinartz, B. and Olivier, H. (2009). Computational studies of the effect of wall temperature on hypersonic shock-induced boundary layer separation. In: Klaus Hannemann and Friedrich Seiler, Shock Waves: Proceedings of the 26th International Symposium on Shock Waves. 26th International Symposium on Shock Waves (ISSW26), Gottingen, Germany, (1231-1236). 15-20 July 2007. doi:10.1007/978-3-540-85181-3_70


Author Brown, L.
Fischer, C.
Boyce, R. R.
Reinartz, B.
Olivier, H.
Title of paper Computational studies of the effect of wall temperature on hypersonic shock-induced boundary layer separation
Conference name 26th International Symposium on Shock Waves (ISSW26)
Conference location Gottingen, Germany
Conference dates 15-20 July 2007
Proceedings title Shock Waves: Proceedings of the 26th International Symposium on Shock Waves
Journal name Shock Waves, Vol 2, Proceedings
Place of Publication Berlin, Germany
Publisher Springer-Verlag Berlin
Publication Year 2009
Sub-type Fully published paper
DOI 10.1007/978-3-540-85181-3_70
ISBN 9783540851806
3540851801
Editor Klaus Hannemann
Friedrich Seiler
Volume 2
Issue Part XIX
Start page 1231
End page 1236
Total pages 6
Language eng
Abstract/Summary This paper shall present the numerical results of an investigation into the effect of wall to freestream temperature on boundary layer separation for a nominal flat plate/ 15degree compression corner. The numerical results will be compared to the experimental results of Bleilebens and Olivier [1]. The major findings from their study showed a distinct trend for boundary layer separation size to increase with wall-to-freestream temperature ratio; that the separation process was dictated purely by laminar effects; and that the separated shear layer transitioned to turbulence during the reattachment process. The transitional behaviour of the reattaching shear layer was characterised in their results through high Stanton number distributions post-reattachment and the observance of Gortler vortices in the infrared thermography images.
Q-Index Code E1
Q-Index Status Provisional Code
Institutional Status Non-UQ

 
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Created: Thu, 26 Mar 2009, 10:43:52 EST by Maryanne Watson on behalf of Faculty Of Engineering, Architecture & Info Tech