High-Speed Diagnostics in a Natural Gas–Air Rotating Detonation Engine-Reference-Cited by-同舟云学术

High-Speed Diagnostics in a Natural Gas–Air Rotating Detonation Engine

Published:2020-07 Issue:4 Volume:36 Page:498-507
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Journell Christopher L.¹,Gejji Rohan M.¹,Walters Ian V.¹,Lemcherfi Aaron I.¹,Slabaugh Carson D.¹,Stout Jeffrey B.²

Affiliation:

1. Purdue University, West Lafayette, Indiana 47907

2. Aerojet Rocketdyne, Inc., Canoga Park, California 91309

Funder

U.S. Department of Energy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.B37740

Reference45 articles.

1. Application of the Continuous Rotating Detonation to Gas Turbine

2. Continuous Spin Detonations

3. Experimental Study of the Performance of a Rotating Detonation Engine with Nozzle

4. StechmannD. P. “Experimental Study of High-Pressure Rotating Detonation Combustion in Rocket Environments,” Doctoral Dissertation, Purdue Univ., West Lafayette, IN, 2017.

5. AndersonW. S.HeisterS. D.HartsfieldC. “Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine,” AIAA Paper 2019-0474, Jan. 2019. 10.2514/6.2019-0474

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