Laser-Induced Plasma Ignition Experiments in a Direct-Connect Supersonic Combustor at Mach 3-Reference-Cited by-同舟云学术

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Laser-Induced Plasma Ignition Experiments in a Direct-Connect Supersonic Combustor at Mach 3

Published:2020-09 Issue:5 Volume:36 Page:732-743
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Baccarella Damiano¹,Lee Gyu Sub¹,Liu Qili¹,Elliott Gregory S.¹,Freund Jonathan B.¹,Lee Tonghun¹

Affiliation:

1. University of Illinois at Urbana-Champaign, Urbana, Illinois 61801

Funder

National Nuclear Security Administration

Air Force Office of Scientific Research

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.B37846

Reference37 articles.

1. Stirred reactor analysis of cavity flame holders for scramjets

2. A study of recessed cavity flowfields for supersonic combustion applications

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

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

5. Cavity Oscillation Mechanisms in High-Speed Flows

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2. Nitric Oxide and Temperature Measurement Using Laser Absorption Spectroscopy in Arc-Heater Plenum;AIAA Journal;2024-09-03

3. Design and analysis of an ideal scramjet flowpath;Physics of Fluids;2024-03-01

4. Investigation of ignition and flame propagation in an axisymmetric supersonic combustor with laser-induced plasma;Physics of Fluids;2023-12-01

5. Flame development prediction of supersonic combustion flow based on lightweight cascaded convolutional neural network;Physics of Fluids;2023-02-01

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