Experimental Investigation of Dynamic Separation for a Hypersonic Inlet Cover in Mach 6 Flow (AIAA 2016-4111)
32nd AIAA aerodynamic measurement technology and ground testing conference 2016 ; 2016 ; Washington D.C
2016-01-01
11 pages
Conference paper
English
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OUTPUT ERROR CONTROL USING R-ADAPTATION (AIAA 2017-4111)
British Library Conference Proceedings | 2017
|DataCite | 1924