Visualization and analysis of bow shocks in a superorbital expansion tube
Author:
Affiliation:
1. University of Queensland, Brisbane 4072, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13376
Reference15 articles.
1. Mach number effects on conical surface features of swept shock-wave/boundary-layer interactions
2. Correlation of Conical Interactions Induced by Sharp Fins and Semicones
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4. Interaction between shock waves and boundary layer induced by a semicone placed on a flat plate.
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1. Experimental Expansion Tube Study of the Flow over a Toroidal Ballute;Journal of Spacecraft and Rockets;2004-09
2. Enhanced flow visualization with near-resonant holographic interferometry;Applied Optics;2003-08-01
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4. Diagnostics of a range of highly superorbital carbon dioxide flows;39th Aerospace Sciences Meeting and Exhibit;2001-01-08
5. Free-Piston Driven Expansion Tubes;Handbook of Shock Waves;2001
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