Flame Structure Characterization in a Dual-Mode Scramjet Using Hydroxyl Planar Laser-Induced Fluorescence
Author:
Affiliation:
1. University of Virginia, Charlottesville, Virginia 22904
2. George Washington University, Washington, District of Columbia 20052
Funder
Directorate for Engineering
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J059465
Reference56 articles.
1. Scramjet Engines: The First Forty Years
2. VinogradovV.KobigskyS.PetrovM. “Experimental Investigation of Liquid Carbonhydrogen Fuel Combustion in Channel at Supersonic Velocities,” AIAA Paper 1992-3429, July 1992. 10.2514/6.1992-3429
3. Characteristics of the Compressible Shear Layer over a Cavity
4. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
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