Approximate boundary conditions for the flow of a mixture of reacting gases

Author:

Schubert B. Schmitt-v.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Reference13 articles.

1. Schaaf, S. A., Chambré, P. L.: Flow of rarefied gases. High Speed Aerodyn. Jet Propulsion3, 687?739 (1958).

2. Clarke, J. F., McChesney, M.: The dynamics of real gases, pp. 119?164 and 244?248. London: Butterworths 1964.

3. Schmitt-v. Schubert, B.: Hypersonic viscous stagnation flow of a gas with vibrational relaxation. DFVLR-AVA, IB 252-74 H 11, 1974. Paper presented at the 9th Int. Symp. on Rarefied Gasdynamics, Göttingen, Germany, 1974.

4. Schmitt-v. Schubert, B.: Vibrational nonequilibrium stagnation shock layers at hypersonic speed and low Reynolds number. Int. J. Heat Mass Transfer21, 1041?1048 (1978).

5. Mitra, N. K., Fiebig, M.: Low Reynolds number vibrational nonequilibrium flow in Laval nozzle. In: Rarefied gasdynamics (Becker, M., Fiebig, M., eds.), B.21. Proc. of the 9th Int. Symp., Göttingen, Germany,1974.

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1. Physico–chemical modelling in hypersonic flow simulation;Progress in Aerospace Sciences;2000-04

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