Burning rate estimation based on flame evolution in a channel-Reference-Cited by-同舟云学术

Burning rate estimation based on flame evolution in a channel

Published:2023-03 Issue: Volume:204 Page:768-775
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Yakovenko Ivan^ORCID,Kiverin Alexey,Krivosheyev Pavel^ORCID,Kuzmitski Viachaslau,Navitski Aliaksei,Penyazkov Oleg,Tyurnin Alexey^ORCID,Yarkov Andrey^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference58 articles.

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2. Fluid mechanics of pulse detonation thrusters;Phylippov;Acta Astronaut.,2012

3. Three-dimensional modeling of rotating detonation in a ramjet engine;Smirnov;Acta Astronaut.,2019

4. 3D numerical modeling of a cylindrical RDE with an inner body extending out of the nozzle;Betelin;Acta Astronaut.,2020

5. Detonative propulsion;Wolański;Proc. Combust. Inst.,2013

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1. Ignition delay of lean hydrogen-air mixtures;International Journal of Hydrogen Energy;2024-05

2. Effect of channel geometry on the flame acceleration and transition to detonation in acetylene-oxygen-nitrogen mixtures;Acta Astronautica;2024-04

3. Acceleration of the Flame in a Smooth Channel and Detonation Transition;Journal of Engineering Physics and Thermophysics;2023-11

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5. Experimental Study of Flame Acceleration Processes and Deflagration-to-Detonation Transition: Review of Works of the A.V. Luikov Heat and Mass Transfer Institute of the National Academy of Sciences of Belarus;Combustion, Explosion, and Shock Waves;2023-08