High-Fidelity Simulations of Pressure-Gain Combustion Devices Based on Detonations-Reference-Cited by-同舟云学术

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High-Fidelity Simulations of Pressure-Gain Combustion Devices Based on Detonations

Published:2017-01 Issue:1 Volume:33 Page:153-162
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Kailasanath K.¹,Schwer D. A.¹

Affiliation:

1. Naval Research Laboratory, Washington, District of Columbia 20375

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.B36169

Reference35 articles.

1. Review of propulsion applications and numerical simulations of the pulsed detonation engine concept

2. EidelmanS.GrossmanW. “Pulse Detonation Engine: Experimental and Theoretical Review,” AIAA Paper 1992-3168, July 1992.

3. Review of Propulsion Applications of Detonation Waves

4. A review of PDE research-performance estimates

5. Recent Developments in the Research on Pulse Detonation Engines

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1. Performance Characterization of a Radial Rotating Detonation Combustor With Axial Exhaust;Journal of Engineering for Gas Turbines and Power;2024-08-23

2. Continuous Injector Geometry Variation to Augment Rotating Detonation Combustor Operation and Performance;Journal of Propulsion and Power;2024-05

3. Influence of Chamber Pressure on Rotating Detonation Modes with Continuously Variable Exit Nozzle Area;AIAA SCITECH 2024 Forum;2024-01-04

4. Performance Characteristics of a Rotating Detonation Combustor Exiting Into a Pressurized Plenum to Simulate Gas Turbine Inlet;Journal of Engineering for Gas Turbines and Power;2023-12-08

5. Effects of droplet evaporation on the flow field of hydrogen-enhanced rotating detonation engines with liquid kerosene;International Journal of Hydrogen Energy;2023-10

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