The atmospheric composition behind a normal shock ahead of a hypersonic vehicle differs from the atmosphere ahead of the shock. Various models of air equilibrium composition are compared, analysis of areas of these models applicability is performed. Numerical simulations of flow in a channel with a step are performed using models of perfect gas and high-temperature air. The results computed with both models are compared.
|Journal||IOP Conference Series: Materials Science and Engineering|
|State||Published - 25 Sep 2020|
|Event||13th International Conference on Applied Mathematics and Mechanics in the Aerospace Industry, AMMAI 2020 - Alushta, Russian Federation|
Duration: 6 Sep 2020 → 13 Sep 2020
Scopus subject areas
- Materials Science(all)