Numerical Analysis for Magnetic Control of Heat-Transfer and Pressure in Hypersonic Shock Wave Interference Flows
Local heat-transfer and pressure increases due to shock wave interference are critical problems in structural designs for complicated hypersonic vehicles. Therefore, many experiments and computational simulations have been done to identify the critical shock interference phenomena [1, 2, 3]. Types of the shock interference were classified by Edney in Ref. . His classification shows that some types are severe interference and the others types are not. The most critical interference is called Type IV.
KeywordsFree Stream Computational Simulation Blunt Body Hypersonic Vehicle Magnetic Control
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