Shock Layer Radiation Analysis using a Hypervelocity Shock Tube (HVST)
نویسندگان
چکیده
منابع مشابه
Shock layer instability near the Newtonian limit of hypervelocity flows
The curved bow shock in hypersonic flow over a blunt body generates a shear layer with smoothly distributed vorticity. The vorticity magnitude is approximately proportional to the density ratio across the shock, which may be very large in hypervelocity flow, making the shear layer unstable. A computational study of the instability reveals that two distinct nonlinear growth mechanisms occur in s...
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ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
سال: 2012
ISSN: 0549-3811
DOI: 10.2322/tjsass.55.37