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首页> 外文期刊>International Journal of Turbo and Jet Engines >Bleeding Control for Improving Internal Waverider Inlet Self-Starting ability
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Bleeding Control for Improving Internal Waverider Inlet Self-Starting ability

机译:改善内部Waverider入口自启动能力的出血控制

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摘要

Internal waverider inlets (IWIs) are novel three-dimensional (3D) high-performance inward turning inlets. However, they possess poor self-starting capacity when applied in a fixed-geometry inlet for ramjets. Firstly, this paper presents an analysis of self-starting capacity for IWIs to demonstrate that IWIs face more difficult challenges when used as ramjet inlets than they do as scramjet inlets. Self-starting capacity must be taken into account when designing ramjet inlets. Secondly, the impact of a fluidic control method on a fixed-geometry IWI was studied by numerical simulation of fluid flow. The numerical results show that the fluidic control mechanism improved the self-starting capacity of the IWI at low Mach numbers: the minimum Mach number of self-starting capacity was reduced from M3.8 to M3.2; furthermore, the compression ratio was increased from 29.9 with no fluidic control to 31.9. By analyzing two different groups of fluidic control positions, it was determined that bleeding before the separation bubble has no impact on the IWI self-starting capacity.
机译:内部Waverider入口(IWI)是新型三维(3D)高性能向内转动入口。然而,当施加在用于拉姆喷嘴的固定几何入口时,它们具有差的自启动能力。首先,本文提出了对IWIS的自我启动能力分析,以证明在用作Ramjet入口时,IWIS的挑战比它们的争夺入口更恰好。在设计Ramjet入口时必须考虑自启动容量。其次,通过流体流动的数值模拟研究了流体控制方法对固定几何IWI的影响。数值结果表明,流体控制机制在低马赫数下改善了IWI的自启动能力:自启动容量的最小马赫数从M3.8降至m3.2;此外,压缩比从29.9增加,没有流体对照至31.9。通过分析两种不同的流体控制位置,确定分离气泡之前的出血对IWI自启动能力没有影响。

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