Cavity Flows in a Scramjet Engine by the Space-Time Conservation and Solution Element Method
Author:
Affiliation:
1. The Ohio State University, Columbus, Ohio 43210-1154
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.9017
Reference21 articles.
1. Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors
2. Analysis of unsteady cavity flows for scramjet applications
3. Effect of Flame-Holding Cavities on Supersonic-Combustion Performance
4. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
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