Characterization of Shock Wave Transfer in a Pulse Detonation Engine–Crossover System-Reference-Cited by-同舟云学术

Characterization of Shock Wave Transfer in a Pulse Detonation Engine–Crossover System

Published:2015-12 Issue:12 Volume:53 Page:3674-3685
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Driscoll Robert¹,St. George Andrew¹,Stoddard William¹,Munday David¹,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.J054045

Reference26 articles.

1. RouserK. “Unsteady Specific Work and Isentropic Efficiency of a Radial Turbine Driven by Pulsed Detonations,” Ph.D. Dissertation, Air Force Institute 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. KaneshigeM.ShepherdJ. “Detonation Database,” Graduate Aerospace Labs. of the California Inst. of Technology TR-FM97-8, Pasadena, CA, 1997.

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