Experimental Study on Combustion Modes in a Supersonic Combustor
Author:
Affiliation:
1. Tokyo Institute of Technology, Yokohama 226-8502, Japan
2. Japan Aerospace Exploration Agency, Kakuda 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.B34020
Reference24 articles.
1. Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane
2. Ramjet Engine Test Facility (RJTF) in NAL-KRC, Japan
3. Mach 6 Testing of a Scramjet Engine Model
4. Mach 8 Testing of a Scramjet Engine Model
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