Open AccessThe tests of a hypersonic module with external flow at M = 4 in hot-shot wind tunnel
Author(s) -
A. V. Starov,
M. I. Yaroslavtsev
Publication year - 2021
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/5.0052256
Subject(s) - hypersonic wind tunnel , transonic , mach number , wind tunnel , nozzle , supersonic wind tunnel , hypersonic speed , inflow , scramjet , aerospace engineering , shot (pellet) , calibration , combustion , subsonic and transonic wind tunnel , expansion tunnel , mechanics , flow (mathematics) , environmental science , materials science , engineering , aerodynamics , physics , chemistry , combustor , organic chemistry , quantum mechanics , metallurgy
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