Oleh G. Shvydkyi 2024. 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. 2, 6 (Jul. 2024), 346–367. DOI:https://doi.org/10.61359/11.2106-2429.