| Abstract: | The features of the flowfield and heat transfer on the surface of an axisymmetric body with a narrow groove in its nose immersed
in a hypersonic perfect-gas stream (M∞=6.1) are studied on the basis of a numerical analysis of the two-dimensional Navier-Stokes equations. The calculations are
performed for both thermally insulated and isothermal surfaces having grooves of different width. The calculated results are
compared with experimental data.
Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 1, pp. 117–124, January–February,
2000.
The study was carried out with the support of the International Scientific and Technical Center (project No. 036). |
