化学非平衡模型对高焓钝楔边界层稳定性分析的影响

李晨辉; 万兵兵; 涂国华; 胡伟波; 陈坚强; 蒋崇文

doi:10.7638/kqdlxxb-2024.0002

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化学非平衡模型对高焓钝楔边界层稳定性分析的影响

研究论文 | 更新时间：2026-05-28

- 化学非平衡模型对高焓钝楔边界层稳定性分析的影响
- Effects of chemical non-equilibrium models on stability analysis of blunt wedge boundary layer with high enthalpy
- 空气动力学学报 2024年42卷第12期页码：12-24
- 作者机构：
  
  1. 北京航空航天大学航空科学与工程学院,北京,100191
  2. 空天飞行空气动力科学与技术全国重点实验室,绵阳,621000
- 作者简介：
  
  李晨辉（1996—），男，河南三门峡人，博士研究生，研究方向：高速边界层转捩. E-mail：lchenh@buaa.edu.cn
  万兵兵*，副研究员，研究方向：高速边界层转捩. E-mail：wanbingbing@tiu.edu.cn
  陈坚强*，研究员，研究方向：高速复杂流动机理. E-mail：chenjq@cardc.cn
- 基金信息：
  
  国家自然科学基金（92052301，12002353，12202473）
- DOI：10.7638/kqdlxxb-2024.0002
  中图分类号： O357.4
- 纸质出版：2024
- 稿件说明：
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李晨辉, 万兵兵, 涂国华, 等. 化学非平衡模型对高焓钝楔边界层稳定性分析的影响[J]. 空气动力学学报, 2024, 42(12): 12−24.

LI Chenhui, WAN Bingbing, TU Guohua, et al. Effects of chemical non-equilibrium models on stability analysis of blunt wedge boundary layer with high enthalpy[J]. 2024, 42(12): 12-24.
李晨辉, 万兵兵, 涂国华, 等. 化学非平衡模型对高焓钝楔边界层稳定性分析的影响[J]. 空气动力学学报, 2024, 42(12): 12−24. DOI： 10.7638/kqdlxxb-2024.0002

LI Chenhui, WAN Bingbing, TU Guohua, et al. Effects of chemical non-equilibrium models on stability analysis of blunt wedge boundary layer with high enthalpy[J]. 2024, 42(12): 12-24. DOI： 10.7638/kqdlxxb-2024.0002.

摘要

对于高马赫数飞行器，其绕流场温度会急剧升高引发高温化学非平衡效应，进而影响边界层转捩过程。针对这一问题，一般需在基本流计算和稳定性分析中引入反映复杂物理化学过程的计算模型，但这制约了计算效率，且不同模型可能会得到不同的稳定性分析结果。为了进一步研究一些工程常用模型对计算的影响，本文发展了化学非平衡流动的线性稳定性分析方法，考察了化学非平衡效应对高焓钝楔边界层稳定性的影响途径，分析了不同热力学、输运系数和化学反应等物理化学模型造成的稳定性分析结果差异。研究表明：化学非平衡效应主要通过改变基本流影响模态

值，转捩预测时可以仅在基本流求解中考虑化学非平衡效应以提高计算效率；物理化学模型对第二模态的影响较小，对于由第二模态主导的转捩过程，预测结果对化学非平衡流动中物理化学模型的选取不敏感，但在第三模态对

值贡献较大时，模型选取对转捩预测结果的影响则无法忽略。

Abstract

Boundary layer transition has a significant impact in the design of flight vehicles. At high Mach numbers

the temperature in the boundary layer rises rapidly

leading to a series of high-temperature effects

which affect the boundary layer transition process. Some physicochemical models are often introduced to reflect these effects in the numerical simulations

which greatly increases the computational cost. In the meantime

different models may give different results in the flow stability analysis. Currently

relevant research in this field is not sufficient

and

the effects of typical physicochemical models have not been considered. In the present study

the linear stability theory (LST) for chemical non-equilibrium flow was developed

and the influence of chemical non-equilibrium effects on the flow stability of blunt wedge boundary layers was investigated. The differences in the boundary layer stability calculation results caused by physicochemical models such as the thermal models

the transport models

and the chemical models were analyzed. The results show that the chemical non-equilibrium effects mainly affect the

factors by changing the basic flow

thus

they can be considered merely in the basic flow calculation in order to improve the computational efficiency. The transition prediction result is insensitive to the selection of physicochemical models for second-mode dominant transition in the chemical non-equilibrium flow. However

when the contribution of the third mode to the

values is large

the influence of physicochemical model on the transition prediction cannot be ignored.

关键词

Keywords

references

CHEN J Q, YUAN X X, TU G H, et al . Recent progresses on hypersonic boundary-layer transition[J ] . Scientia Sinica (Physica, Mechanica Astronomica), 2019 , 49 ( 11 ): 125 − 138 (in Chinese).

DUAN Y, YAO S Y, LI S Y, et al . Review of progress in some issues and engineering application of hypersonic boundary layer transition[J ] . Acta Aerodynamica Sinica, 2020 , 38 ( 2 ): 391 − 403 (in Chinese).

ANDERSON J D. Hypersonic and high temperature gas dynamics[M]. New York: Mcgraw-Hill Book Company, 1988: 596−599.

MALIK M R, ANDERSON E C . Real gas effects on hypersonic boundary-layer stability[J ] . Physics of Fluids A, 1991 , 3 ( 5 ): 803 − 821 .

STUCKERT G, REED H L . Linear disturbances in hypersonic, chemically reacting shock layer[J ] . AIAA Journal, 1994 , 32 ( 7 ): 1384 − 1393 .

HUDSON M L, CHOKANI N, CANDLER G V . Linear stability of hypersonic flow in thermochemical nonequilibrium[J ] . AIAA Journal, 1997 , 35 ( 6 ): 958 − 964 .

FAN Y, WAN B B, HAN Y F, et al . Hydrodynamic stability and transition prediction with the chemical equilibrium gas model[J ] . Journal of Aerospace Power, 2016 , 31 ( 7 ): 1658 − 1668 (in Chinese).

CHEN X L, FU S . Linear stability analysis of hypersonic boundary layer on a flat-plate with thermal-chemical non-equilibrium effects[J ] . Acta Aerodynamica Sinica, 2020 , 38 ( 2 ): 316 − 325 (in Chinese).

WANG Z, HAN Y F, CAO W . Effects of entropy layer on the boundary layer over hypersonic blunt cones considering chemical reactions[J ] . Physics of Fluids, 2023 , 35 ( 3 ): 034111 .

DEMANGE S, QADRI U A, JUNIPER M P, et al . Global modes of viscous heated jets with real gas effects[J ] . Journal of Fluid Mechanics, 2022 , 936 : A7 .

ZANUS L, PINNA F . Evolution of instability modes in Mach 10 frozen and chemically reacting boundary layers by means of non-linear parabolized stability equations[J ] . Physics of Fluids, 2021 , 33 ( 6 ): 064106 .

CHEN X L, WANG L, FU S . Parabolized stability analysis of hypersonic thermal-chemical nonequilibrium boundary-layer flows[J ] . AIAA Journal, 2021 , 59 ( 7 ): 2382 − 2395 .

CHEN X L, WANG L, FU S . Energy transfer of hypersonic and high-enthalpy boundary layer instabilities and transition[J ] . Physical Review Fluids, 2022 , 7 ( 3 ): 033901 .

CHEN X L, WANG L, FU S . Secondary instability of the hypersonic high-enthalpy boundary layers with thermal-chemical nonequilibrium effects[J ] . Physics of Fluids, 2021 , 33 ( 3 ): 034132 .

MARXEN O, MAGIN T E, SHAQFEH E S G, et al . A method for the direct numerical simulation of hypersonic boundary-layer instability with finite-rate chemistry[J ] . Journal of Computational Physics, 2013 , 255 : 572 − 589 .

LIU P X, LI C, SUN D, et al . Statistical characteristics of high-temperature turbulent boundary layer considering chemical non-equilibrium effect[J ] . Acta Aerodynamica Sinica, 2022 , 40 ( 4 ): 124 − 131 (in Chinese).

MA Y B, ZHONG X L. Receptivity to freestream disturbances of a Mach 10 nonequilibrium reacting oxygen flow over a flat plate[C]// 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virigina: AIAA, 2004: AIAA 2004-256.

ADAM P H, HORNUNG H G . Enthalpy effects on hypervelocity boundary-layer transition: ground test and flight data[J ] . Journal of Spacecraft and Rockets, 1997 , 34 ( 5 ): 614 − 619 .

GRONVALL J E, JOHNSON H B, CANDLER G V . Boundary-layer stability analysis of the high enthalpy shock tunnel transition experiments[J ] . Journal of Spacecraft and Rockets, 2014 , 51 ( 2 ): 455 − 467 .

GUPTA R N, YOS J M, THOMPSON R A, et al. A review of reaction rates and thermodynamic and transport properties for the 11-species air model for chemical and thermal nonequilibrium calculations to 30000 K, NASARP-1232 [R]. NASA, 1990.

PARK C. Nonequilibrium hypersonic aerothermodynamics[M]. New York: Wiley-Interscience, 1990.

DUNN M G, KANG S. Theoretical and experimental studies of reentry plasmas: NASA-CR-2232 [R]. NASA, 1973.

BROKAW R S . Approximate formulas for the viscosity and thermal conductivity of gas mixtures[J ] . The Journal of Chemical Physics, 1958 , 29 ( 2 ): 391 − 397 .

SARMA G S R . Physico-chemical modelling in hypersonic flow simulation[J ] . Progress in Aerospace Sciences, 2000 , 36 ( 3-4 ): 281 − 349 .

TU G H, CHEN J Q, YUAN X X, et al . Progress in flight tests of hypersonic boundary layer transition[J ] . Acta Mechanica Sinica, 2021 , 37 ( 11 ): 1589 − 1609 .

LI P, CHEN J Q, DING M S, et al . Framework design of NNW-HyFLOW hypersonic flow simulation software[J ] . Acta Aeronautica et Astronautica Sinica, 2021 , 42 ( 9 ): 625718 (in Chinese).

GAO Z X, JIANG C W, LI C X . Review of numerical simulation methods for hypersonic and high-enthalpy non-equilibrium flow[J ] . Advances in Mechanics, 2023 , 53 ( 3 ): 561 − 591 (in Chinese).

BRENNER G, GERHOLD T, HANNEMANN K, et al . Numerical simulation of shock/shock and shock-wave/boundary-layer interactions in hypersonic flows[J ] . Computers Fluids, 1993 , 22 ( 4-5 ): 427 − 439 .

Brenner G, Prinz U. Numerical simulation of chemical and thermal nonequilibrium flows behind compression shocks[C]// 27th Thermophysics Conference. Nashville. Reston, Virigina: AIAA, 1992: AIAA-92–2879.

ZENG M, HANG J, LIN Z B, et al . Numerical analysis of the effects of different thermo-chemical nonequilibrium models on hypersonic nozzle flow[J ] . Acta Aerodynamica Sinica, 2006 , 24 ( 3 ): 346 − 349 (in Chinese).

GAO T S, DONG W Z, DING M S, et al . The effects of physicochemical models on distribution of plasma in high temperature flowfield[J ] . Acta Aerodynamica Sinica, 2013 , 31 ( 5 ): 541 − 545,553 (in Chinese).

CHEN W F, SUN J H, TIAN D Y, et al . Influence of physical and chemical models on electromagnetic scattering characteristics of flow field[J ] . Acta Aeronautica et Astronautica Sinica, 2023 , 44 ( 12 ): 58 − 67 (in Chinese).

LYTTLE I, REED H. Sensitivity of second-mode linear stability to constitutive models within hypersonic flow[C]// 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virigina: AIAA, 2005: AIAA 2005-889.

FRANKO K J, MACCORMACK R W, LELE S K. Effects of chemistry modeling on hypersonic boundary layer linear stability prediction[C]//40th Fluid Dynamic Conference and Exhibit. Chicago, Illinois. Reston, Virigina: AIAA, 2010: AIAA 2010-4601.

WAN B B, HAN Y F, FAN Y, et al . Effect of transport properties of high-temperature air on bound ary layer stability and transition prediction[J ] . Journal of Aerospace Power, 2017 , 32 ( 1 ): 188 − 195 (in Chinese).

MIRÓ MIRÓ F, BEYAK E S, PINNA F, et al . High-enthalpy models for boundary-layer stability and transition[J ] . Physics of Fluids, 2019 , 31 ( 4 ): 044101 .

SUTTON K, GNOFFO P A . Multi-component diffusion with application to computational aerothermodynamics[J ] . 7th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, Albuquerque. Reston, Virigina: AIAA, 2005 : AIAA-98 − 2575 .

VAN LEER B. Flux-vector splitting for the Euler equations[C]//8th International Conference on Numerical Methods in Fluid Dynamics, Heidelberg, Berlin: Springer, 1982: 507-512.

JIANG G S, SHU C W . Efficient implementation of weighted ENO schemes[J ] . Journal of Computational Physics, 1996 , 126 ( 1 ): 202 − 228 .

MALIK M R . Numerical methods for hypersonic boundary layer stabil ity[J ] . Journal of Computational Physics, 1990 , 86 ( 2 ): 376 − 413 .

HUDSON M L. Linear stability of hypersonic flows in thermal and chemical nonequilibrium[D]. Raleigh, North Carolina: North Carolina State University, 1996.

VINCENTI W G, KRUGER C H. Introduction to physical gas dynamics[M]. Malabar: Krieger, 1975.

EHLERS J G, GORDON S, HEIMEL S, et al. Thermodynamic properties to 6000K for 210 substances involving the first 18 elements: NASA-SP-3001 [R]. NASA, 1963.

BLOTTNER F G, JOHNSON M, ELLIS M. Chemically reacting viscous flow program for multi-component gas mixtures: SC-RR--70-754[R]. Office of Scientific and Technical Information (OSTI), 1971.

WILKE C R . A viscosity equation for gas mixtures[J ] . Journal of Chemical Physics, 1950 , 18 ( 4 ): 517 − 519 .

WAN B B, TU G H, YUAN X X, et al . Identification of traveling crossflow waves under real hyperson ic flight conditions[J ] . Physics of Fluids, 2021 , 33 ( 4 ): 044110 .

WAN B B, CHEN J Q, YUAN X X, et al . Three-dimensional receptivity of a blunt-cone boundary layer to incident slow acoustic waves[J ] . AIAA Journal, 2022 , 60 ( 8 ): 4523 − 4531 .

MIRÓ MIRÓ F, PINNA F, BEYAK E S, et al. Diffusion and chemical non-equilibrium effects on hypersonic boundary-layer stability[C]// 2018 AIAA Aerospace Sciences Meeting, Kissimmee, Florida. Reston, Virigina: AIAA, 2018: AIAA 2018-1824.

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