Investigation of Combustion Characteristics in a Kerosene-Fueled Supersonic Combustor with Air Throttling-Reference-Cited by-同舟云学术

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Investigation of Combustion Characteristics in a Kerosene-Fueled Supersonic Combustor with Air Throttling

Published:2020-12 Issue:12 Volume:58 Page:5379-5388
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Tian Ye¹,Le Jialing¹,Yang Shunhua¹,Zhong Fuyu¹

Affiliation:

1. Science and Technology on Scramjet Laboratory, China Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China

Funder

CARDC Fundamental and Frontier Technology Research Fund

Postdoctoral Research Foundation of China

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference29 articles.

1. Supersonic Combustion in Air-Breathing Propulsion Systems for Hypersonic Flight

2. Dual-Pump Coherent Anti-Stokes Raman Scattering Measurements in a Supersonic Combustor

3. Mixing and Combustion Characteristics of Kerosene in a Model Supersonic Combustor

4. Simulation of Supersonic Combustion Involving H2/Air and C2H4/Air

5. Finite Rate Chemistry Large-Eddy Simulation of Self-Ignition in Supersonic Combustion Ramjet

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4. Investigation on compression ramp with surface V-groove for scramjet combustor;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2024-08-28

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