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International Journal of Fluid Mechanics Research
ESCI SJR: 0.206 SNIP: 0.446 CiteScore™: 0.9

ISSN Imprimir: 2152-5102
ISSN En Línea: 2152-5110

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International Journal of Fluid Mechanics Research

DOI: 10.1615/InterJFluidMechRes.v36.i1.40
pages 64-79

Design and Development of Electromagnetic Shockwave Control Experiment

Xiaoqing (Cathy) Qian
Department of Mechanical Engineering, P.O. Box 1163, Alabama A&M University, Huntsville, AL 35762, USA
Zhengtao Deng
Department of Mechanical Engineering, P.O. Box 1163, Alabama A&M University, Huntsville, AL 35762, USA
Ron Litchford
NASA Marshall Space Flight Center, Huntsville, AL 35812, USA
John Foote
NASA Marshall Space Flight Center, Huntsville, AL 35812, USA
John Lineberry
LyTec LLC, Tullahoma, Tennessee 37388, USA
V. A. Bityurin
LyTec LLC, Tullahoma, Tennessee 37388, USA

SINOPSIS

Initial development of an experimental program on electromagnetic control of shockwave was presented. This experiment was aimed to investigate the validity of the potential MHD flow control for hypersonic flight vehicle. Experimental arc heater facility modification, test model design and analysis, cradle design and preliminary experimental results were reported. Shockwave locations for high Mach number ionized flows over a spherical nose-cone with cylindrical body and with an applied magnetic field was reported. Results provide excellent platform to simulate electromagnetic shockwave control for the hypersonic flight by introducing ionization seed into the airflow and generates artificial re-entry conditions at reduced Mach number.


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