Aerodynamic Characterization of a Cavity Flameholder in a Premixed Dual-Mode Scramjet-Reference-Cited by-同舟云学术

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Aerodynamic Characterization of a Cavity Flameholder in a Premixed Dual-Mode Scramjet

Published:2018-05 Issue:3 Volume:34 Page:739-749
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Kirik Justin W.,Goyne Christopher P.,McDaniel James C.,Rockwell Robert D.,Cantu Luca M. L.,Gallo Emanuela C. A.,Cutler Andrew D.

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/pdf/10.2514/1.B36605

Reference43 articles.

1. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview

2. Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors

3. Supersonic Combustion Experiments with a Cavity-Based Fuel Injector

4. Mixing and Combustion Studies Using Cavity-Based Flameholders in a Supersonic Flow

5. Research on supersonic combustion

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2. Dynamic response characteristics of flame during condition transition in a cavity-based scramjet combustor;Acta Astronautica;2023-10

3. Upgraded design methodology for airframe/engine integrated full-waverider vehicle considering thrust chamber design;Acta Astronautica;2023-10

4. Simulated Scramjet Shock Train Control Using an All-Coefficient Adaptive Control Approach;Journal of Propulsion and Power;2023-07

5. Direct numerical simulation of supersonic internal flow in a model scramjet combustor under a non-reactive condition;Physics of Fluids;2023-02-01

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