Design of an Asymmetric Scramjet Nozzle with Circular to Rectangular Shape Transition
Author:
Affiliation:
1. Department of Power Engineering, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
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.B34949
Reference29 articles.
1. A Century of Ramjet Propulsion Technology Evolution
2. Design of Three-Dimensional Hypersonic Inlets with Rectangular-to-Elliptical Shape Transition
3. Advanced Computational-Fluid-Dynamics Techniques for Scramjet Combustion Simulation
4. Measurement of Flow Properties and Thrust on Scramjet Nozzle Using Pressure-Sensitive Paint
5. Thrust Nozzle Design Study for a Quasi-Axisymmetric Scramjet-Powered Vehicle
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