Open AccessTesting of hydrogen-fueled detonation ramjet in aerodynamic wind tunnel at Mach 1.5 and 2.0
Author(s) -
В. И. Звегинцев,
V. S. Ivanov,
С. М. Фролов,
И. О. Шамшин,
А. Э. Зангиев
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 - 10.1063/5.0051978
Subject(s) - mach number , ramjet , detonation , aerospace engineering , deflagration , aerodynamics , specific impulse , deflagration to detonation transition , thrust , boiler blowdown , wind tunnel , combustion , total air temperature , mechanics , engineering , environmental science , mechanical engineering , physics , inlet , combustor , chemistry , explosive material , organic chemistry
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