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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.
Abstract
The slip conditions for a multicomponent mixture with diffusion, wall-catalyzed atom recombination and thermal radiation are derived. The more realistic multicomponent species slip conditions are shown to be necessary for accurate merged shock layer solutions on a sphere. These slip conditions are used in a first-order similarity solution of the Navier-Stokes equations with nonequilibrium chemistry for the merged shock layer. Results of this quick numerical solution are compared with a time dependent solution around the sphere and with measured arc jet results at low Reynolds numbers. The similarity solution, unlike the time dependent solution, shows smooth radial profiles of the pressure and smooth variations of velocity slip, skin friction, temperature slip and heat transfer around the body. The present first-order similarity solution is valid up to 25 deg from the stagnation point and takes less than 1% of the computer time to run a time dependent scheme. The smaller stand-off distance obtained from the similarity solution is supported by experimental data. The measured heat flux is closer to the similarity solution than the time dependent method at the stagnation point and shows the proper variation with circumferential angle up to at least 40 deg.

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Citations
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Journal ArticleDOI

Slip boundary conditions on a catalytic surface in a multicomponent gas flow

B. A. Kiryutin, +1 more
- 01 Jan 1996 - 
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

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

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.
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