Combustion of Vaporized Kerosene in Supersonic Model Combustors with Dislocated Dual Cavities-Reference-Cited by-同舟云学术

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Combustion of Vaporized Kerosene in Supersonic Model Combustors with Dislocated Dual Cavities

Published:2014-09 Issue:5 Volume:30 Page:1152-1160
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Zhang Taichang¹,Wang Jing¹,Fan Xuejun¹,Zhang Peng²

Affiliation:

1. State Key Laboratory of High Temperature Gas Dynamics, Chinese Academy of Sciences, 100190 Beijing, People’s Republic of China

2. Department of Mechanical Engineering, Hong Kong Polytechnic University, Kowloon, Hong Kong, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35096

Reference29 articles.

1. Investigation of Vaporized Kerosene Injection in a Supersonic Model Combustor

2. Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor

3. Thermal Effects on Fuel Injection in a Swirl-Stabilized Gas Turbine Combustor

4. Flame-Holding Configurations for Kerosene Combustion in a Mach 1.8 Airflow

5. Supersonic Combustion Experiments with a Cavity-Based Fuel Injector

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