Investigations of injection parameters on combustion oscillation in a supersonic crossflow-Reference-Cited by-同舟云学术

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Investigations of injection parameters on combustion oscillation in a supersonic crossflow

Published:2018-11 Issue: Volume:152 Page:426-436
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Zhao Guo-Yan,Sun Ming-Bo,Wang Ya-Nan,Li Xi-Peng,Wang Hong-Bo

Funder

National Natural Science Foundation of China

Innovative Sustentation Fund for Excellent Ph.D. Students in Hunan province

China Scholarship Council

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Spark ignition process in a scramjet combustor fueled by hydrogen and equipped with multi-cavities at Mach 4 flight condition;Sun;Exp. Therm. Fluid Sci.,2012

2. Design Manual of Aviation Engine;Chen,2000

3. Combustion oscillations in a scramjet engine combustor with transverse fuel injection;Choi;Proc. Combust. Inst.,2005

4. Experimental investigation on laser-induced plasma ignition of hydrocarbon fuel in scramjet engine at takeover flight conditions;Li;Acta Astronaut.,2017

5. Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholder;Wang;Proc. Combust. Inst.,2013

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1. On scale effect of supersonic combustion in axisymmetric combustor;Aerospace Science and Technology;2024-09

2. Role of cavity in a Mach 8 axisymmetric scramjet combustor: Flame stabilization vs combustion enhancement;Physics of Fluids;2024-01-01

3. Experimental investigations of combustion oscillation modes in a large-aspect-ratio dual-mode combustor equipped with multi-strut;Physics of Fluids;2023-10-01

4. Effect of boundary layer thickness on supersonic combustion in a scramjet combustor;Aerospace Science and Technology;2023-08

5. Combustion Oscillations in Scramjet Combustor with Different Fuel Injection Schemes;AIAA Journal;2023-05

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