Development of some hypersonic benchmark flows using CFD and experiment

Hillier, R., Boyce, R. R., Creighton, S. A., Fiala, A., Jackson, A. P., Mallinson, S. G., Sheikh, A. H., Soltani, S. and Williams, S. (2003) Development of some hypersonic benchmark flows using CFD and experiment. Shock Waves Journal, 12 5: 375-384. doi:10.1007/s00193-003-0179-0


Author Hillier, R.
Boyce, R. R.
Creighton, S. A.
Fiala, A.
Jackson, A. P.
Mallinson, S. G.
Sheikh, A. H.
Soltani, S.
Williams, S.
Title Development of some hypersonic benchmark flows using CFD and experiment
Journal name Shock Waves Journal   Check publisher's open access policy
ISSN 0938-1287
Publication date 2003-03-01
Sub-type Article (original research)
DOI 10.1007/s00193-003-0179-0
Open Access Status
Volume 12
Issue 5
Start page 375
End page 384
Total pages 10
Place of publication Berlin
Publisher Springer - Verlag
Language eng
Subject 090107 Hypersonic Propulsion and Hypersonic Aerodynamics
Abstract This paper presents a set of test cases in high speed aerodynamics that describe our perceived relationship between experiment and computation. Computational fluid dynamics, with sensible interpretation, can guide experimental design, so that wind tunnel studies can focus better on fundamental ‘benchmark’ studies. Likewise experimental data may be used as feed back to evaluate codes and to improve their physical modelling. Here we present several test cases, developed in our laboratory, that we regard as basic ‘building blocks’ for high speed aerodynamics. These include: design for boundary-layer/pressure-gradient interaction; cavity flows; shock-wave/boundary-layer interactions; techniques for a graduated and controlled study of three-dimensional separated flows.
Q-Index Code C1
Q-Index Status Provisional Code
Institutional Status Unknown

Document type: Journal Article
Sub-type: Article (original research)
Collections: Faculty of Engineering, Architecture and Information Technology Publications
Excellence in Research Australia (ERA) - Collection
 
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