A Comprehensive Study of Combustion Oscillations in a Hydrocarbon-Fueled Scramjet Engine
Author:
Affiliation:
1. The Pennsylvania State University
2. Taitech, Inc.
3. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-836
Reference16 articles.
1. Analysis of Dual-Mode Hydrocarbon Scramjet Operation at Mach 4-6.5
2. Combustion oscillations in a scramjet engine combustor with transverse fuel injection
3. The Response of Normal Shocks in Diffusers
4. Newly Developed Direct-Connect High-Enthalpy Supersonic Combustion Research Facility
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