Numerical Simulations in Scramjet Combustion with Boundary-Layer Bleeding
Author:
Affiliation:
1. Tohoku University, Miyagi 980-8579, Japan
2. Japan Aerospace Exploration Agency, Miyagi 981-1525, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.7967
Reference28 articles.
1. Dual-Mode Combustion of Hydrogen in a Mach 5, Continuous-Flow Facility
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