Supplementary File

Title Fig. 9. The longitudinal component of velocity along line s1 (a) and line s2 (b).
Submission Numerical simulation of the interaction between weak shock waves and supersonic boundary layer on a flat plate with the blunt leading edge
Type author.submit.suppFile.figureResearchMaterials
Date 2025-03-23
Language ru

Supplementary File

File Name 266742-627873-1-SP.jpg
Original file name IMZIG-2024-02-09-9.jpg
File Size 140KB
Date uploaded 23.03.2025 08:13