Experimental study on the wall temperature and heat transfer of a two-phase pulse detonation rocket engine-Reference-Cited by-同舟云学术

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Experimental study on the wall temperature and heat transfer of a two-phase pulse detonation rocket engine

Published:2017-03 Issue: Volume:114 Page:387-393
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Wang Yongjia,Wang Ke,Fan Wei,He Jiannan,Zhang Yang,Zhang Qibin,Yao Kuiguang

Funder

National Natural Science Foundation of China

Doctorate Program Foundation of Education Ministry of China

Innovation Foundation for Doctor Dissertation of Northwestern Polytechnical University

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference28 articles.

1. Pulse detonation engine theory and concepts;Bussing;Prog. Astronaut. Aeronaut.,1996

2. Pulse detonation propulsion: challenges, current status, and future perspective;Roy;Prog. Energy Combust. Sci.,2004

3. Experimental investigation of an air-breathing pulse detonation turbine prototype engine;Qiu;Appl. Therm. Eng.,2016

4. Semi-free-jet simulated experimental investigation on a valveless pulse detonation engine;Wang;Appl. Therm. Eng.,2014

5. Performance analysis of the pulse detonation rocket engine based on constant volume cycle model;Li;Appl. Therm. Eng.,2010

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4. Impact of nozzles on the wall-temperature in a valveless pulse detonation engine;Experimental Thermal and Fluid Science;2023-08

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