29th International Symposium on Shock Waves 2 2015
DOI: 10.1007/978-3-319-16838-8_63
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Incident Shock-Transverse Jet Interactions at Mach 1.9: Effect of Different Jet Gases

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“…The same wind tunnel was also employed in a wide range of supersonic flow related studies [15,23,24,25,27,28,29,30,31,32,33]. The test section of the wind tunnel has dimensions of 485.5 mm (length) × 150 mm (width) × 216.5 mm (height).…”
Section: Methodsmentioning
confidence: 99%
“…The same wind tunnel was also employed in a wide range of supersonic flow related studies [15,23,24,25,27,28,29,30,31,32,33]. The test section of the wind tunnel has dimensions of 485.5 mm (length) × 150 mm (width) × 216.5 mm (height).…”
Section: Methodsmentioning
confidence: 99%