Three-dimensional effects on line-of-sight visualization measurements of supersonic and hypersonic flow over cylinders

Author:

Eichmann Troy N.,McIntyre Timothy J.,Bishop Alexis I.,Vakata Sosefo,Rubinsztein-Dunlop Halina

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Reference19 articles.

1. AeroSoft Inc.: GASP, The General Aerodynamic Simulation Program. Aerosoft Inc., Blacksburg, Virginia (1997)

2. Austin, J.M., Jacobs, P.A., Kong, M.C., Barker, P., Littleton, B.N., Gammie, R.: The Small Shock Tunnel Facility at UQ. Department of Mechanical Engineering Report 2/97, The University of Queensland, Brisbane (1997)

3. Bishop, A.I.: Spectrally Selective Holographic Interferometry Techniques for Flow Diagnostics. PhD Thesis, The University of Queensland, Brisbane (2001)

4. Bishop A.I., Littleton B.N., McIntyre T.J. and Rubinsztein-Dunlop H. (2001). Near-resonant holographic interferometry of hypersonic flow. Shock Waves 11(1): 23–29

5. Boyce R.R., Morton J.W., Houwing A.F.P., Mundt C. and Bone D.J. (1996). Computational fluid dynamics validation using multiple interferometric views of a hypersonic flowfield. J. Spacecr. Rockets 33(3): 319–325

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