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Steering Moments Creation in Supersonic Flow by Off-Axis Plasma Heat Addition

机译:通过离轴等离子体热添加产生超音速流中的转向力矩

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摘要

The change in aerodynamic forces as a result of local plasma heat addition to supersonic flow (Mach 3.0), upstream of a cone, is studied numerically by solving the three-dimensional compressible Euler equations. In principle, such an effect on the forces and moments can be used for vehicle steering as well as drag reduction. Local energy addition to the flow is achieved by the use of microwave radiation as a heating-source and an electron beam to control the air conductivity and consequently the location of the energy deposition. This approach requires heating only in a localized preionized region, and so the strength of the microwave field has to be much lower than the critical value of the electric field at breakdown. Results show the potential effects of heat addition on the aerodynamic forces. The corresponding power and the optimized location required to achieve these effects are discussed.
机译:通过求解三维可压缩的Euler方程,对由于局部等离子热量加到圆锥上游的超声速流动(马赫3.0)而引起的空气动力变化进行了数值研究。原则上,这种对力和力矩的影响可以用于车辆转向以及减阻。通过使用微波辐射作为加热源和电子束来控制空气的传导性,进而控制能量沉积的位置,可以实现向流中添加局部能量。这种方法只需要在局部预离子化区域加热,因此微波场的强度必须远低于击穿时电场的临界值。结果显示了热量添加对空气动力的潜在影响。讨论了实现这些效果所需的相应功率和优化位置。

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