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Fluid-thermal coupled investigation on the combinational spike and opposing/lateral jet in hypersonic flows

机译:在超声波流动中的组合尖峰和相对/横向射流的流体热耦合研究

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摘要

The drag reduction and thermal protection mechanism induced by the spike and its combinations with jet strategy is investigated in the current study. A fluid-thermal coupled analysis is carried out to explore the impacts of the jet pressure ratio (PR), the length-to-diameter ratio (L/D) of the spike and the lateral jet location (D-L) on the peak pressure and peak heat flux of the blunt head. The obtained results suggest that the combined spike and multi-jet strategy is the most promising technology for the drag and heat reduction. The increases in jet pressure ratios including opposing jet ratio and lateral jet ratio are advantageous and provide the maximum reduction in the drag and heat flux. Specifically, for the cases of PRo = 0.2 and PRo = 0.6, the peak heat fluxes are decreased by about 2.25 kW/m(2) and 0.37 kW/m(2) respectively after 0.6 s', and the decrease rate becomes more slowly during the coupling process. Further, the negative thrust produced by the opposing jet plays a key role in the total drag component. For the L/D effect, the peak pressure and drag coefficient decreases when L/D increases. However, it is noteworthy that when L/D = 0.5, the peak heat flux is close to that when L/D = 2, which, is at a relatively low level of 104.83 kW/m(2). In addition, the lateral jet location has a decisive influence on the flow structure, drag coefficient and heat flux distribution, and DL = 8 mm gives the minimum drag and heat flux while the peak pressure is the maximum.
机译:目前研究研究了由尖峰诱导的减压和热保护机制及其与喷射策略的组合。进行流体热耦合分析以探讨喷射压力比(PR),尖峰的长度比(L / D)和横向喷射位置(DL)对峰值压力的影响钝头的峰值热通量。所获得的结果表明,组合的尖峰和多喷射策略是最有前途的阻力和散热的技术。喷射压力比,包括相反的喷射比和横向喷射比的增加是有利的,并且提供阻力和热通量的最大降低。具体地,对于Pro = 0.2和Pro = 0.6的情况,峰热通量分别在0.6 s'之后分别降低约2.25kW / m(2)和0.37kW / m(2),减少速度变得更加缓慢在耦合过程中。此外,由相对喷射产生的负推点在总阻力分量中起着关键作用。对于L / D效应,当L / D增加时,峰值压力和拖动系数降低。然而,值得注意的是,当L / D = 0.5时,峰值热通量接近,当L / D = 2时,其在相对较低的104.83 kW / m(2)中。另外,横向喷射位置对流动结构,拖曳系数和热通量分布具有决定性的影响,DL = 8mm表示最小的拖动和热通量,而峰值压力是最大值。

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