Oxygen concentration distribution in a pulse detonation engine with nozzle–ejector combinational structures
Author:
Affiliation:
1. School of Power and Energy, Northwestern Polytechnical University, Xi’an, China
2. Aero Engine Academy of China, Beijing, China
3. Beijing Space Pioneer Aerospace Technology Co., Ltd., Beijing, China
Abstract
Funder
National Natural Science Foundation of China
Natural Science Foundation of Shanxi Province of China
Technology Foundation for Selected Overseas Scholar of Shanxi Province of China
Fundamental Research Funds for the Central Universities
Seed Foundation of Innovation and Creation for Graduate Students in Northwestern Polytechnical University
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/0954410021991284
Reference21 articles.
1. Reactive impulse from the explosion of a gas mixture in a semiinfinite space
2. The Effect of Nozzles and Extensions on Detonation Tube Performance
3. Analysis of an Ejector-Augmented Pulse Detonation Rocket
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1. Computational Analysis of Shrouded Ejector Effect on Starting Vortex and Combustion Efficiency in Pulse Detonation Combustor with Different Fuels;Combustion Science and Technology;2023-11-16
2. A State of Art Review on Thermodynamics Performance Analysis in Pulse Detonation Combustor;Applications of Calorimetry;2022-06-23
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