Research on validation and verification of Chinese transport model CHN-T1

ZHANG Jinwei; ZHANG Xiaoliang; SUN Xiaoling; QI Shu'ni

doi:10.7638/kqdlxxb-2018.0216

English Version Journal Login

您当前的位置：

首页 >

文章列表页 >

Research on validation and verification of Chinese transport model CHN-T1

更新时间：2026-05-28

- Research on validation and verification of Chinese transport model CHN-T1
- Vol. 37, Issue 2, Pages: 320-328(2019)
- 作者机构：
  
  中国航空工业空气动力研究院,沈阳,110034
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2018.0216
  CLC： V211.3
- Published：2019
- 稿件说明：
移动端阅览
章锦威, 张小亮, 孙晓玲, 戚淑妮. 运输机标模CHN-T1的验证确认计算研究[J]. 空气动力学学报, 2019, 37(2): 320-328.

ZHANG Jinwei, ZHANG Xiaoliang, SUN Xiaoling, et al. Research on validation and verification of Chinese transport model CHN-T1[J]. 2019, 37(2): 320-328.
章锦威, 张小亮, 孙晓玲, 戚淑妮. 运输机标模CHN-T1的验证确认计算研究[J]. 空气动力学学报, 2019, 37(2): 320-328. DOI： 10.7638/kqdlxxb-2018.0216.

ZHANG Jinwei, ZHANG Xiaoliang, SUN Xiaoling, et al. Research on validation and verification of Chinese transport model CHN-T1[J]. 2019, 37(2): 320-328. DOI： 10.7638/kqdlxxb-2018.0216.

摘要

采用自研的非结构混合网格解算器CARIA-OVERSET对我国第一届航空CFD可信度研讨会提供的运输机标模CHN-T1进行了验证确认计算。重点研究了网格形式、网格尺度、湍流模型等对运输机标模CHN-T1的总体气动特性、局部流场特征、压力分布以及计算收敛性等的影响，并把计算结果与风洞试验数据进行比较分析。分析结果表明，非结构混合网格解算器的计算结果与风洞试验数据吻合度较好。在固定升力条件下，非结构网格的网格尺度误差大于结构网格，湍流模型对迎角和俯仰力矩的影响较大，翼身结合处的分离特性模拟差异较小。带支撑构型的全机升力和低头力矩增加、阻力减小，机翼静气弹变形后升力、阻力和低头力矩均减小。全湍和自由转捩模型的计算结果存在一定差异，差异随着雷诺数的增大而变小。

Abstract

Chinese transport model CHN-T1 is provided by the first aviation CFD credibility seminar in China. 3D flow simulations were accomplished with the unstructured hybrid grids and the flow solver CARIA-OVERSET for the validation and verification study of the CHN-T1. The effects of mesh type

mesh size

and turbulence model were studied on the overall aerodynamic characteristics

flow field characteristics

pressure distribution. It is shown that the numerical results are in good agreement with the wind tunnel test data. Under the condition of fixed lift

the grid scale error of unstructured grids is larger than that of structured grids. Turbulence model has great impact on pitch moment

while weak influence on the separation characteristics at wing-body junction with support configuration

the lift and the pitch down moment of the CHN-T1 model increase

while drag decreases. In consideration of the aeroelastic deformation

the lift

the drag and pitch down moment decrease. The results with full turbulence model and free transition model are different

but the difference decreases with increasing Reynolds number.

关键词

Keywords

references

LEVY D W, et al. Summary of data from the first AIAA CFD drag prediction workshop[C]. 40th AIAA AerospaceSicences Meeting Exhibit, Reno, Nevada, 2002.

LAFLIN K R, et al. Data summary of from the second AIAA CFD drag prediction workshop[J]. Journal of Aircraft, 2005, 42(6):1165-1178.

VASSBERG J C, et al. Abridged summary of the third AIAA CFD drag prediction workshop[J]. Journal of Aircraft, 2008, 45(6):781-798.

VASSBERG J C, et al. Summary of the fourth AIAA CFD drag prediction workshop: AIAA 2010-4547[R]. Reston: AIAA, 2010.

LEVY D W, et al. Summary of data from the fifth AIAA CFD drag prediction workshop: AIAA 2013-0046[R]. Reston: AIAA, 2013.

KEYE S, et al. DPW-6 summary of participant data test case 5 CRM WB coupled aero-structural simulation[C]. 6th AIAA CFD drag prediction workshop, Washington, D C, 2016.

NPARC. NPARC alliance CFD verification validation[DB].[2016-02-05]. <a href="http://www.grc.nasa.gov/www/wind/valid/" target=_blank>http://www.grc.nasa.gov/www/wind/valid/

LIANG Y H, ZHU Y, ZHU C, et al. Analyze platform of CFD reliability-wise CFD[C]//12th National Computational Fluid Dynamics Conference. Xi'an: Chinese Aeronautics Computation Technique Reserch Institute, AVIC 2004: 775-780. (in Chinese).

Bai W, LI L. CFD V V and open benchmark database[J]. Chinese Journal of Aeronautics, 2006, 19(2):160-167.

DENG X G, ZONG W G, ZHANG L P, et al. Verification and validation in computational fluid dynamics[J]. Advances in Mechanics, 2007, 37(2):279-288. (in Chinese).

CHEN S S, LIU L Y, YAN C, et al. Design and realization of automated testing cloud platform for CFD verification and validation[J]. Acta Aeronautica of Astronautica Sinica, 2017, 38(3):120209. (in Chinese)

LI Q, LIU D W, XU X, et al. Experimental study of aerodynamic characteristics of CHN-T1 standard model in 2.4 m transonic wind tunnel[J]. Acta Aerodynamica Sinica, 2019, 37(2):337-342. (in Chinese)

LANGTRY R B. MENTER F R. Transition modeling for general CFD applications in aeronautics[C]. 43rd AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2005-522. Reno, Nevada: 2005.

LANGTRY R B. MENTER F R. Correlation-based transition modeling for unstructured parallelized computational fluid dynamics codes[J]. AIAA Journal, 2009, 47(12):2894-2906.

YU Y G, ZHOU Z, HUANG J T, et al. Design of aerodynamic standard CHN-T1 for single channel passenger aircraft[J]. Acta Aerodynamica Sinica, 2018, 36(3):505-513. (in Chinese)

ZHANG Y B, TANG J, CHEN J T, et al. Aerodynamic characteristics prediction of CHN-T1 standard model with unstructured grid[J]. Acta Aerodynamica Sinica, 2019, 37(2):262-271. (in Chinese)

LI W, WANG Y T, HONG J W, et al. Aerodynamic characteristics Simulation of CHN-T1 Model with TRIP3.0[J]. Acta Aerodynamica Sinica, 2019, 37(2):272-279. (in Chinese)

KANG S, et al. Error analysis and grid convergence of CFD simulation[J]. Journal of Engineering Thermophysics, 2010, 31(12):2009-2013. (in Chinese)

STERN F, WILSON R V, et al. Comprehensive approach to verification and validation of CFD simulations, Part1:Methodology and Procedures[J]. ASME Journal of Fluids Engineering, 2001, 123:793-802.

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Static aerodynamic characteristics of symmetrical wind turbine airfoils considering the influence of near-ocean underlying surface

Aerodynamic characteristics of combined wing-tip link UAV

Aerodynamic characteristics of seagull bionic airfoil based on breathable structure

Impact of key area optimization on the aerodynamic characteristics of a high-speed train in crosswind

Numerical simulation of liquid film cooling on hypersonic oblique plate

Related Author

Jia Xiaofeng

Huang Wen

Hu Chuanxin

Xu Xinye

Wang Han

Xu Xiaoping

Wang Guichen

Li Yunlong

Related Institution

School of urban construction, Wuhan University of Science and Technology, Wuhan

School of Aeronautics, Northwestern Polytechnical University, Xi’an

National Key Laboratory of Aircraft Configuration Design, Xi’an

School of Aeronautics, Northwestern Polytechnical University, Xi'an

National Key Laboratory of Aircraft Configuration Design, Xi'an

AI问答

⁰