Ramp Injector Scale Effects on Supersonic Combustion
Author:
Affiliation:
1. School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana 47906
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.B34716
Reference12 articles.
1. WhiteF., Viscous Fluid Flow, 3rd ed., McGraw–Hill, New York, 2006, pp. 505–570.
2. Evaluation of parallel injector configurations for Mach 2 combustion
3. In-Stream Hypermixer Fueling Pylons in Supersonic Flow
4. Supersonic mixing and combustion control using streamwise vortices
5. Investigation of a contoured wall injector for hypervelocity mixing augmentation
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