Effect of Wall Temperature on Hypersonic Gas Flow Past a Compression Ramp Using Quasi-Gas Dynamic Equations. Journal of Aviation Science and Technology (ISSN: 2815-5661), [S. l.], v. 1, n. 2, 2026. Disponível em: https://ojs.vaajast.org/index.php/jast/article/view/73.. Acesso em: 17 apr. 2026.