Open AccessPreliminary experimental results of heat flux surface field registration at the hypersonic aerodynamic shock tube using temperature sensitive paint
Author(s) -
V. E. Mosharov,
Vladimir Radchenko,
I V Senuev,
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 - 10.1088/1742-6596/1009/1/012036
Subject(s) - aerodynamic heating , hypersonic speed , aerodynamics , shock tube , materials science , aerospace engineering , heat flux , tube (container) , expansion tunnel , shock (circulatory) , flux (metallurgy) , mechanics , hypersonic flow , field (mathematics) , shock wave , heat transfer , physics , composite material , engineering , medicine , mathematics , pure mathematics , metallurgy