Control of detonation combustion in a high-velocity gas mixture flow

DOI10.1134/S0081543818010091zbMath1460.76915OpenAlexW2803127864MaRDI QIDQ721432

D. Kharzeev

Publication date: 19 July 2018

Published in: Proceedings of the Steklov Institute of Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0081543818010091

zbMATH Keywords

detonation wavestoichiometric hydrogen-air mixturesupersonic channel flowthrust-producing flow

Mathematics Subject Classification ID

Combustion (80A25) Reaction effects in flows (76V05) Supersonic flows (76J20) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Cites Work

• Unnamed Item
• Stability of gas mixture flow with a stabilized detonation wave in a plane channel with a constriction
• Numerical modeling of detonation combustion of hydrogen-air mixtures in a convergent-divergent nozzle
• Stabilization of detonation combustion of a high-velocity combustible gas mixture flow in a plane channel
• Investigation of certain techniques for stabilizing detonationwaves in a supersonic flow

This page was built for publication: Control of detonation combustion in a high-velocity gas mixture flow