Shock tunnel and numerical studies of a large inlet-fuelled inward turning axisymmetric scramjet
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference
2012-01-01
Conference paper
Electronic Resource
English
SHOCK TUNNEL AND NUMERICAL STUDIES OF A LARGE INLET-FUELLED INWARD TURNING AXISYMMETRIC SCRAMJET
British Library Conference Proceedings | 2012
|Investigation of the Effects of Lateral Cowl Length in an Inward Turning Scramjet Inlet
British Library Conference Proceedings | 2013
|