Shock wave induced flow past a circular cylinder in a dusty-gas shock tube.
نویسندگان
چکیده
منابع مشابه
Nonequilibrium Real-gas Effects on Disturbance/bow Shock Interaction in Hypersonic Flow past a Cylinder
The interaction of free-stream disturbances and the bow shock wave in hypersonic ow past a blunt leading edge is an important part of hypersonic boundary layer receptivity to free-stream disturbances. It has been shown that, for a perfect gas, the back and forth interaction and reeection of acoustic waves behind the shock greatly amplify the magnitudes of the disturbance waves. The interaction ...
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ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
سال: 1987
ISSN: 0387-5016,1884-8346
DOI: 10.1299/kikaib.53.3533