Article
Heat and Mass Transfer and Physical Gasdynamics
2013. V. 51. № 2. P. 231–245
Surzhikov S.T.
Convective heating of small-radius spherical blunting for relatively low hypersonic velocities
Annotation
The chemically and thermally nonequilibrium air flow over a spherically blunted cylinder for velocities within M=6–18 with free-stream parameters corresponding to the altitudes of 22 and 37 km is considered. The cylinder bluntness radius is varied within Rn=0.66–5.08 cm. The initial data are chosen on the basis of a series of experimental data on convective heating of the leading critical point of spherical bluntness. These experimental data are in good agreement with the results of numerical simulation.
Article reference:
Surzhikov S.T. Convective heating of small-radius spherical blunting for relatively low hypersonic velocities, High Temp., 2013. V. 51. № 2. P. 231
Surzhikov S.T. Convective heating of small-radius spherical blunting for relatively low hypersonic velocities, High Temp., 2013. V. 51. № 2. P. 231