arXivDaily arXiv每日学术速递 周一至周五更新
北美退伍军人节(Veterans Day),12 日无更新
arXiv 2501.05074physics.flu-dyn
收藏

稀薄环境中的横向湍流射流

Lateral turbulent jet in rarefied environment

Songyan Tian, Lei Wu, Minping Wan

AI总结:

本研究采用结合SST湍流模型与GSIS稀薄气体方法的GSIS-SST,分析50–80 km高度横向射流中湍流与稀薄效应的耦合影响,揭示二者对俯仰力矩、热通量和剪切应力预测的显著差异。

摘要:

横向射流在控制高超声速飞行器的轨迹和气动加热方面起着关键作用。然而,湍流效应与稀薄效应之间的复杂相互作用很少得到研究。本研究通过采用新开发的GSIS-SST方法[J. Fluid Mech. 1002 (2025) A10]填补了这一知识空白,该方法结合了用于湍流的剪切应力输运(SST)模型和用于稀薄气体流动的通用合成迭代格式(GSIS)。研究发现,在50 km至80 km的高度,GSIS-SST与纯GSIS(SST)之间俯仰力矩的最大相对差异达到28%(20%)。虽然射流本应降低表面热通量,但其湍流显著削弱了这种降低,例如,当射流压力比为1.5时,GSIS-SST预测的热通量比GSIS高约一个数量级。增大迎角会增强局部湍流,导致GSIS-SST与GSIS之间在剪切应力和热通量方面的差异扩大。这些认识增进了我们对横向射流流动的理解,并凸显了在中空高超声速飞行中同时考虑湍流效应和稀薄效应的重要性。

英文摘要:

Lateral jets play a crucial role in controlling the trajectory and aerodynamic heating of hypersonic vehicles. However, the complex interaction between turbulent and rarefaction effects has rarely been examined. This study fills this knowledge gap by employing the newly developed GSIS-SST method [J. Fluid Mech. 1002 (2025) A10], which combines the shear stress transport (SST) model for turbulent flow and the general synthetic iterative scheme (GSIS) for rarefied gas flow. It is found that, at altitudes from 50 km to 80 km, the maximum relative difference in the pitch moment between the GSIS-SST and pure GSIS (SST) reaches 28% (20%). While the jet is supposed to reduce the surface heat flux, its turbulence significantly diminishes this reduction, e.g., the GSIS-SST predicts a heat flux about one order of magnitude higher than the GSIS when the jet pressure ratio is 1.5. Increasing the angle of attack intensifies local turbulence, resulting in expanded discrepancies in shear stress and heat flux between GSIS-SST and GSIS. These insights enhance our comprehension of lateral jet flows and highlight the importance of accounting for both turbulent and rarefaction effects in medium-altitude hypersonic flight.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

↑