Evaluation of Shock Dividers using Numerical and Experimental Methods-Reference-Cited by-同舟云学术

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Evaluation of Shock Dividers using Numerical and Experimental Methods

Published:2020-01-05 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2020 Forum
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Author:

Rezay Haghdoost Mohammad¹,Thethy Bhavraj S.²,Nadolski Maikel³,Klein Rupert³,Honnery Damon²,Edgington-Mitchell Daniel M.²,Seo Bonggyun¹,Paschereit Christian O.¹,Oberleithner Kilian¹

Affiliation:

1. Technical University of Berlin

2. Monash University

3. Free University of Berlin

Publisher

American Institute of Aeronautics and Astronautics

Reference47 articles.

1. Review on Recent Advances in Pulse Detonation Engines

2. A review of research on pulse detonation engine nozzles

3. The Thermodynamic and Fluid Dynamic Functions of a Pulsed Detonation Engine Nozzle

4. Performance Estimations of a Pulse Detonation Engine with Exit Nozzle

Cited by 3 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. Kiel Probes for Stagnation Pressure Measurement in Rotating Detonation Combustors;AIAA Journal;2022-06

2. Computational Simulation of an Exhaust Plenum Charged by a Multi-tube Pulsed Detonation Combustor;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2021-11-13

3. Mitigation of Pressure Fluctuations From an Array of Pulse Detonation Combustors;Journal of Engineering for Gas Turbines and Power;2021-03-31

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