The limits of applicability of continuum flow models in the problem of the hypersonic rarefied gas flow over blunt bodies are determined by an asymptotic analysis of the Navier-Stokes equations, the numerical solution of the viscous shock layer equations and the numerical and asymptotic solution of
โฆ LIBER โฆ
Hypersonic flows of rarefied gas
โ Scribed by M.N. Kogan
- Publisher
- Elsevier Science
- Year
- 1962
- Tongue
- English
- Weight
- 820 KB
- Volume
- 26
- Category
- Article
- ISSN
- 0021-8928
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