Open AccessPreliminary experimental assessment of supersonic airflow behavior over ExoMars and X–43 inlet models using multiple flow regime shock tube
Author(s) -
M. A. Kоtov,
L. B. Ruleva,
S. I. Solodovnikov,
С. Т. Суржиков
Publication year - 2018
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1009/1/012038
Subject(s) - shock tube , aerodynamics , supersonic speed , mach number , airflow , shock (circulatory) , shock wave , aerospace engineering , inlet , hypersonic speed , tube (container) , mechanics , spacecraft , flow (mathematics) , bow shock (aerodynamics) , choked flow , environmental science , physics , geology , mechanical engineering , engineering , thermodynamics , medicine