Experimental and numerical investigation on initial flame kernel blow-out in a supersonic combustor with a rear-wall-expansion cavity flameholder-Reference-Cited by-同舟云学术

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Experimental and numerical investigation on initial flame kernel blow-out in a supersonic combustor with a rear-wall-expansion cavity flameholder

Published:2019-11 Issue: Volume:164 Page:358-365
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Wang Taiyu,Yang Yixin,Wang Zhenguo,Cai Zun,Sun Mingbo,Li Guangxin

Funder

National Natural Science Foundation of China

Postdoctoral Innovation Talent Support Program of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Recent Research Progress on unstart mechanism, detection and control of hypersonic inlet;Chang;Prog. Aerosp. Sci.,2017

2. Parametric study of fuel distribution effects on a kerosene-based scramjet combustor;Yang;Inter. J. Aerosp. Eng.,2016

3. Prediction dynamic model of shock train with complex background waves;Li;Phys. Fluids,2017

4. Research progress on strut-equipped supersonic combustors for scramjet application;Chang;Prog. Aerosp. Sci.,2018

5. Mixing and combustion studies using cavity-based flameholders in a supersonic flow;Gruber;J. Propuls. Power,2004

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1. Performance study of a central reentrant step pilot-flameholder in a dual-mode combustor;Aerospace Science and Technology;2024-04

2. Experimental Study on Combustion Modes and Oscillations in a Cavity-Based Scramjet Combustor;AIAA Journal;2023-12-09

3. Three-dimensional measurements and analysis of early-stage non-premixed flame development following spark ignition;Aerospace Science and Technology;2023-11

4. Behaviors of the reacting flowfield during the spontaneous formation of ramjet mode under a supersonic inflow;Physics of Fluids;2023-02-01

5. Performance evaluation for scramjet based on ground direct-connected test: A method investigation;Aerospace Science and Technology;2021-10

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