Open AccessShock-wave structures of prospective combined jet engine
Author(s) -
Karina E. Savelova,
Mariya M. Alekseeva,
С. А. Матвеев,
М. В. Чернышов
Publication year - 2021
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 - 10.1088/1742-6596/1959/1/012043
Subject(s) - detonation , mach reflection , shock (circulatory) , mach number , jet (fluid) , shock wave , mechanics , jet engine , reflection (computer programming) , combustion , mach wave , physics , computer science , aerospace engineering , engineering , chemistry , programming language , organic chemistry , explosive material , medicine
The paper presents numerical analysis of typical model flows with Mach reflection. For example, flows in narrowing channels between two triangles and long narrowing channels are discussed. The obtained results can serve as reference data for various approximate theoretical models, in particular, for a newly proposed approximate analytical model, which should take into account combustion and detonation.