Indraft Supersonic Wind Tunnel for Shock Train Investigations
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Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-44866-4_107
Reference44 articles.
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4. Weiss, A., Grzona, A., Olivier, H.: Behavior of shock trains in a diverging duct. Exp. Fluids 49 (2), 355–365 (2010)
5. Reinartz, B.U., Herrmann, C.D., Ballmann, J.: Performance analysis of a hypersonic inlet isolator using computation and experiment. J. Propuls. Power 19 (5), 868–875 (2003)
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1. Development of unsteady background-oriented schlieren system in an indraft supersonic wind tunnel;Journal of Physics: Conference Series;2021-02-01
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