Single-Cycle Unsteady Nozzle Phenomena in Pulse Detonation Engines-Reference-Cited by-同舟云学术

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Single-Cycle Unsteady Nozzle Phenomena in Pulse Detonation Engines

Published:2007-03 Issue:2 Volume:23 Page:325-337
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Owens Zachary C.¹,Hanson Ronald K.¹

Affiliation:

1. Stanford University, Stanford, California 94305

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/10.2514/1.22415

Reference37 articles.

1. System Performance and Thermodynamic Cycle Analysis of Airbreathing Pulse Detonation Engines

2. Thermodynamic Cycle Analysis of Pulse Detonation Engines

3. Constant Volume Limit of Pulsed Propulsion for a Constant ? Ideal Gas

4. Model for the Performance of Airbreathing Pulse-Detonation Engines

Cited by 27 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Study on operation and propulsion features of a pulse detonation rocket engine with secondary oxidizer injection;Applied Thermal Engineering;2020-11

2. Experimental study on the detonation process of a pulse detonation engine with ionized seeds;Defence Technology;2020-02

3. Performance modeling of pulse detonation engines using the method of characteristics;Aerospace Science and Technology;2019-05

4. Diagnostic method based on spontaneous emission to evaluate the detonation cycle;Experimental Thermal and Fluid Science;2019-04

5. A novel blast-mitigation concept for light tactical vehicles;International Journal of Numerical Methods for Heat & Fluid Flow;2017-04-03

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