The Effect of Applied Magnetic Fields on Supersonic Flows over a Backward Facing Step
Author:
Affiliation:
1. Department of Aerospace Engineering, Wichita State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3237
Reference20 articles.
1. Smith, H. E. "The Flow Field and Heat Transfer Downstream of a Rearward Facing Step in Supersonic Flow", ARL-67-0056,March1967.
2. Fletcher, D. G., and McDaniel, J. C. "Quantitative Measurement of Transverse Injector and Free Stream Interaction in aNonreacting Scramjet CombustorUsing LaserInduced Fluorescence",AIAA-1987-0087,1987.
3. McDaniel, J. C., Fletcher,D.G.,Hartfield R. J.,andHollo,S.D. "StagedTransverseInjection into Mach2 Flow behind a Rearward-Facing-Step: A 3-D, Compressible Flow Test Case for Hypersonic Combustor CFD Validation", AIAA-1992-0827,1992.
4. Planar measurement technique for compressible flows using laser-induced iodine fluorescence
5. Petrie, H. L., Samimy, M., and Addy, A. L. "A Study of Compressible Turbulent Free Shear Layers Using Laser DopplerVelocimetry",AIAA-1985-0177,1985.
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1. Temperature and Stress Distributions within a Body in High Speed Flow with and without Applied Magnetic Field;38th Plasmadynamics and Lasers Conference;2007-06-15
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