Numerical study of detonation propagation under the action of supersonic pulsating flow in expanding combustor-Reference-Cited by-同舟云学术

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Numerical study of detonation propagation under the action of supersonic pulsating flow in expanding combustor

Published:2023-10 Issue: Volume:211 Page:25-36
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Dai Jian^ORCID,Liu Jindian

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference54 articles.

1. Mixing enhancement of multi hydrogen jets through the cavity flameholder with extended pylon;Li;Acta Astronaut.,2020

2. Interplay of self-throttling and air throttling on combustion enhancement of the scramjet combustor;Chakravarthy;Acta Astronaut.,2022

3. Numerical investigation on implication of strut profile on combustion characteristics in a cavity based scramjet combustot;Suneetha;Acta Astronaut.,2020

4. Flow structures of a lobed mixer and effects of streamwise vortices on mixing enhancement;Fang;Phys. Fluids,2019

5. Numerical study on reflection of an oblique detonation wave on an outward turning wall;Wang;Phys. Fluids,2020

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. The influence of supersonic spatial-temporal coupling disturbance on detonation in an expanded chamber;Aerospace Science and Technology;2024-04

2. Effect of unsteady supersonic flow on detonation under different hot jet initiation conditions;International Journal of Hydrogen Energy;2024-01

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