C-γ-Reθ高超声速三维边界层转捩预测模型

doi:10.7527/S1000-6893.2021.25711

Abstract

Abstract: To meet the need for hypersonic three-dimensional boundary layer transition prediction for the National Numerical Windtunnel (NNW) Project, we study the hypersonic cross-flow transition criterion and the transition model. The hypersonic database is expanded using the linear stability theory of the e^N method, a fully-localized hypersonic cross-flow transition criterion constructed combining the cross flow strength and surface roughness, a cross-flow extension of the hypersonic modified γ-Re_θ transition model conducted based on the Chant 2.0 computing platform, and a C-γ-Re_θ transition model suitable for hypersonic 3D boundary layer transition prediction established. The transition model is used to predict the cross-flow transition on hypersonic sharp cones in multiple states, and the predicted results are in good accordance with the experimental results.

Key words: National Numerical Windtunnel Project, hypersonic flow, 3D boundary layer, cross-flow transition, transition model

CLC Number:

V211.3

XIANG Xinghao, ZHANG Yifeng, YUAN Xianxu, TU Guohua, WAN Bingbing, CHEN Jianqiang. C-γ-Re_θ model for hypersonic three-dimensional boundary layer transition prediction[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(9): 625711-625711.

References

[1] 陈坚强, 涂国华, 张毅锋, 等. 高超声速边界层转捩研究现状与发展趋势[J]. 空气动力学学报, 2017, 35(3):311-337. CHEN J Q, TU G H, ZHANG Y F, et al. Hypersnonic boundary layer transition:What we know, where shall we go[J]. Acta Aerodynamica Sinica, 2017, 35(3):311-337(in Chinese).
[2] 向星皓, 张毅锋, 陈坚强, 等. 横流转捩模型研究进展[J]. 空气动力学学报, 2018, 36(2):254-264, 180. XIANG X H, ZHANG Y F, CHEN J Q, et al. Progress in transition models for cross-flow instabilities[J]. Acta Aerodynamica Sinica, 2018, 36(2):254-264, 180(in Chinese).
[3] 王亮. 高超音速边界层转捩的模式研究[D]. 北京:清华大学, 2008. WANG L. Modeling flow transition in hypersonic boundary layer[D]. Beijing:Tsinghua University, 2008(in Chinese).
[4] 周玲, 阎超, 郝子辉, 等. 转捩模式与转捩准则预测高超声速边界层流动[J]. 航空学报, 2016, 37(4):1092-1102. ZHOU L, YAN C, HAO Z H, et al. Transition model and transition criteria for hypersonic boundary layer flow[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(4):1092-1102(in Chinese).
[5] ZHANG Y F, ZHANG Y R, CHEN J Q, et al. Numerical simulations of hypersonic boundary layer transition based on the flow solver Chant 2.0[C]//21st AIAA International Space Planes and Hypersonics Technologies Conference. Reston:AIAA, 2017.
[6] 徐晶磊, 宋友富, 张扬, 等. 用于可压缩自由剪切流动的湍流混合长度[J]. 航空学报, 2016, 37(6):1841-1850. XU J L, SONG Y F, ZHANG Y, et al. Turbulence mixing length for compressible free shear flows[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(6):1841-1850(in Chinese).
[7] 陈坚强. 国家数值风洞工程(NNW)关键技术研究进展[J/OL]. 中国科学:技术科学, (2021-04-28)[2021-04-28]. https://kns.cnki.net/kcms/detail/11.5844.TH.202104-28.0914.006.html. CHEN J Q. Advances in the key technologies of Chinese National Numerical Wind Tunnel Project[J/OL]. Scientia Sinica Technologica, (2021-04-28)[2021-04-28]. https://kns.cnki.net/kcms/detail/11.5844.TH.202104-28.0914.006.html (in Chinese).
[8] LANGTRY R B. A correlation-based transition model using local variables for unstructured parallelized CFD codes[D]. Stuttgart:University of Stuttgart, 2006.
[9] 赵磊. 高超声速后掠钝板边界层横流定常涡失稳的研究[D]. 天津:天津大学, 2017. ZHAO L. Study on instability of stationary crossflow vortices in hypersonic swept blunt plate boundary layers[D]. Tianjin:Tianjin University, 2017(in Chinese).
[10] 向星皓, 张毅锋, 陈坚强, 等. 横流转捩模型参数不确定度量化分析与应用研究[J]. 宇航学报, 2020, 41(9):1141-1150. XIANG X H, ZHANG Y F, CHEN J Q, et al. Uncertainty quantification analysis and application research on cross-flow transition model parameters[J]. Journal of Astronautics, 2020, 41(9):1141-1150(in Chinese).
[11] REED H L, HAYNES T S. Transition correlations in three-dimensional boundary layers[J]. AIAA Journal, 1994, 32(5):923-929.
[12] LANGTRY R. Extending the γ-Re_θt local correlation based transition model for crossflow effects[C]//45th AIAA Fluid Dynamics Conference. Reston:AIAA, 2015.
[13] RONALD RADEZTSKY J J R, REIBERT M, SARIC W, et al. Effect of micron-sized roughness on transition in swept-wing flows[C]//31st Aerospace Sciences Meeting. Reston:AIAA, 1993.
[14] 陈久芬, 凌岗, 张庆虎, 等. 7°尖锥高超声速边界层转捩红外测量实验[J]. 实验流体力学, 2020, 34(1):60-66. CHEN J F, LING G, ZHANG Q H, et al. Infrared thermography experiments of hypersonic boundary-layer transition on a 7° half-angle sharp cone[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(1):60-66(in Chinese).
[15] DINZL D J, CANDLER G V. Direct simulation of hypersonic crossflow instability on an elliptic cone[J]. AIAA Journal, 2017, 55(6):1769-1782.
[16] 张毅锋, 向星皓, 万兵兵, 等. 一种基于稳定性方法的横流转捩实验数据拓展技术:CN111380663A[P]. 2020-07-07. ZHANG Y F, XIANG X H, WAN B B, et al. Cross flow transition experimental data expansion technology based on stability method:CN111380663A[P]. 2020-07-07(in Chinese).
[17] XIANG X H, REN H J, ZHANG Y F, et al. Transition prediction with hypersonic cross-flow model on HIFiRE-5[J]. Journal of Physics:Conference Series, 2021, 1786:012051.

C-γ-Re_θ model for hypersonic three-dimensional boundary layer transition prediction

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C-γ-Reθ model for hypersonic three-dimensional boundary layer transition prediction

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C-γ-Re_θ model for hypersonic three-dimensional boundary layer transition prediction