Shock-Initiated Combustion in an Airbreathing, Pulse Detonation Engine-Crossover System-Reference-Cited by-同舟云学术

Shock-Initiated Combustion in an Airbreathing, Pulse Detonation Engine-Crossover System

Published:2016-03 Issue:3 Volume:54 Page:936-949
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Driscoll Robert¹,Randall Steven¹,St. George Andrew¹,Anand Vijay¹,Gutmark Ephraim J.¹

Affiliation:

1. University of Cincinnati, Cincinnati, Ohio 45221

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054571

Reference27 articles.

1. RouserK. “Unsteady Specific Work and Isentropic Efficiency of a Radial Turbine Driven by Pulsed Detonations,” Ph.D. Dissertation, Air Force Inst. of Technology, Wright–Patterson AFB, OH, 2012.

2. Experimental Investigations of the Performance of a Multitube Pulse Detonation Turbine System

3. Experimental Comparison of Axial Turbine Performance Under Steady and Pulsating Flows

4. Thermodynamic Cycle Analysis of Pulse Detonation Engines

5. Impact of DDT Mechanism, Combustion Wave Speed, Temperature, and Charge Quality on Pulsed-Detonation-Engine Performance

Cited by 15 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. The Effect of Ozone Kinetic Enhancement on Detonation Transition in a Microchannel with Dimethyl Ether Mixture;AIAA SCITECH 2024 Forum;2024-01-04

2. Accelerated ignition-shock coupling and deflagration to detonation transition by ozone kinetic enhancement of dimethyl ether mixture;Proceedings of the Combustion Institute;2024

3. Experimental research of the performance and pressure gain in continuous detonation engines with aerospike nozzles;Aerospace Science and Technology;2023-09

4. Quantification of Rotating Detonations Using OH* Chemiluminescence at Varied Widths;AIAA Journal;2021-07

5. Unsteady Effects on NOx Measurements in Pulse Detonation Combustion;Flow, Turbulence and Combustion;2021-03-04