Proceedings ArticleDOI
A similarity solution of the Navier-Stokes equations with wall catalysis and slip for hypersonic, low Reynolds number flow over spheres
TLDR
In this paper, the slip conditions for a multicomponent mixture with diffusion, wall-catalyzed atom recombination and thermal radiation are derived for accurate merged shock layer solutions on a sphere.Citations
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Journal ArticleDOI
Slip boundary conditions on a catalytic surface in a multicomponent gas flow
B. A. Kiryutin,G. A. Tirskii +1 more
TL;DR: In this paper, the boundary conditions for the velocity slip and temperature and concentration jumps on the surface of a body in a rarefied multicomponent gas flow are obtained, and the mathematical treatment is given in detail because of the need to examine critically some previous results which disagree with each other.
Proceedings ArticleDOI
Comparison of viscous-shock-layer heating analysis with Shuttle flight data in slip flow regime
J. L. Shinn,A. L. Simmonds +1 more
TL;DR: In this paper, a comparison of STS-2 Shuttle flight heating data along the windward centerline has been made with two-dimensional nonequilibrium viscous shock-layer solutions obtained with shock and wall-slip conditions at an altitude range of 90 to 110 km.
Journal ArticleDOI
Effect of wall accommodation on heat transfer and pressure in the stagnation region of blunt bodies
Journal ArticleDOI
Vibrational nonequilibrium stagnation shock layers at hypersonic speed and low reynolds number
TL;DR: In this paper, the authors studied the flow field near the stagnation streamline of a plane or axisymmetric blunt body in the merged layer regime using the continuum approach, where the velocity slip and the jump of the translational and rotational temperature as well as that of the vibrational temperature were taken into account.
Slip effects in hypersonic rarefied flow
TL;DR: In this article, a comparison of flowfield calculations for hypersonic flight in the high-altitude rarefied air flow regime has been made to isolate slip-flow effects at the body surface, together with the influence of a relatively thick shock transition region.