Vibrational nonequilibrium stagnation shock layers at hypersonic speed and low reynolds number
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference19 articles.
1. Hypersonic Flow Theory;Hayes,1959
2. Hypersonic viscous flow near the stagnation streamline of a blunt body, Part 1: A test of local similarity, Part 2: Third-order boundary-layer theory and comparison with other methods;Kao;AIAA Jl,1964
3. Merged stagnation shock layer of a nonequilibrium dissociating gas;Chung;AIAA Jl,1968
4. Merged layer ionization in the stagnation region of a blunt body;Lee,1967
5. Computation of nonequilibrium merged stagnation shock lavers by successive accelerated replacement;Dellinger;AIAA Jl,1971
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1. Analogy Between Vibrational and Chemical Nonequilibrium Effects on Stagnation Flows;AIAA Journal;2020-05
2. Theoretical modeling of heat transfer to flat plate under vibrational excitation freestream conditions;International Journal of Heat and Mass Transfer;2020-04
3. Approximate boundary conditions for the flow of a mixture of reacting gases;Acta Mechanica;1995-09
4. Review of German work on controlled re-entry technology;Progress in Aerospace Sciences;1983-01
5. Effects of vibrational relaxation of multi-atomic molecules on stagnation heat transfer;International Journal of Heat and Mass Transfer;1980-12
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