OLEH G. SHVYDKYI. Analytical Solution to the Steady Navier-Stokes Equation for a Supersonic Cone in the Area of Boundary Layer Behind the Shock Wave by Means Tunnel Mathematics. Acceleron Aerospace Journal, [S. l.], v. 2, n. 6, p. 346–367, 2024. DOI: 10.61359/11.2106-2429. Disponível em: https://acceleron.org.in/index.php/aaj/article/view/144. Acesso em: 27 dec. 2024.