Numerical and Experimental Tests of a Supersonic Inlet with Pylon Set and Fuel Injection through Pylons
Author:
Affiliation:
1. Hampton University
2. The George Washington University
3. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-1032
Reference10 articles.
1. Internal designs application for inlet and nozzle aeroperformance improvement
2. Gilinsky, M. M., Khaikine, V., Akyurtlu, A., Akyurtlu, J., etal, "Numerical and Experimental Tests of a Super-sonic Inlet Utilizing a Pylon Set for Mixing, Combustion and Thrust Enhancement," AIAA - 2005 - 3290.
3. Gilinsky, M. M., Gonor, A. L., Khaikine, V. and Blankson, I. M. "Supersonic Inlet with Pylon Set and Star-Shaped Forebody for Mixing, CombustionandThrust Enhancement," AIAA- 2003 -7044.
4. Impact of Axial Vortices on Mixing at a High Convective Mach Number
5. Comparison of Physical and Aerodynamic Ramps as Fuel Injectors in Supersonic Flow
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1. Design and Analysis of Fuel Injector for Efficient Fuel Flow;SAE Technical Paper Series;2024-02-23
2. Numerical Simulations of the Performance of Scramjet Engine Model with Pylon Set Located in the Inlet;Computational Fluid Dynamics 2010;2011
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