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Analyzing of Internal Waverider Inlet and Sidewall Compression Inlet Performance

机译:内部波状进气道和侧壁压缩进气道性能分析

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A new internal waverider inlet which has regular rectangular shape of entrance and exit is designed at M=6.0. It's based on ICFC basic flowfield and derived with the technology of stream tracing and shock cutting. Comparisons are made between the newly designed inlet and a typical sidewall compression inlet. The design Mach number and entrance shape of this new inlet are chosen according to the sidewall compression inlet. Numerical results show that most of the performance parameters of the internal waverider inlet are a bit higher than the sidewall inlet, such as the flow capture coefficient, total pressure recovery and the kinetic efficiency. The paper compares the performance of these two inlets at off-design points as well, the internal waverider inlet can capture more than 91% of incoming flow at all conditions simulated, and shows a better performance either. This paper proves that internal waverider inlet using special technologies which lead to three dimensional compression as well as high flow capture coefficient is a kind of fixed-geometry inlet with great performance.
机译:在M = 6.0处设计了一个新的内部行波器入口,入口和出口具有规则的矩形形状。它基于ICFC基本流场,并采用流跟踪和冲击切割技术衍生。在新设计的进气口和典型的侧壁压缩进气口之间进行了比较。根据侧壁压缩进气口选择新进气口的设计马赫数和入口形状。数值结果表明,内部吸波器入口的大多数性能参数都比侧壁入口高一些,例如流量捕获系数,总压力回收率和动力学效率。本文还比较了这两个进气口在非设计点的性能,在所有模拟条件下,内部行波器进气口都能捕获超过91%的进入流量,并且显示出更好的性能。本文证明,采用特殊技术的内部波状进气口可产生三维压缩,并具有较高的流量捕获系数,是一种性能优良的固定几何进气口。

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