HiLiftPW-3高升力构型数值模拟

doi:10.7527/S1000-6893.2018.22391

Abstract

Abstract: Based on the Reynolds-averaged Navier-Stokes equations and cross-grid technology, this paper adopts the second-order MUSCL-Roe scheme and SA turbulence model to simulate two kinds of high-lift configurations from HiLiftPW-3. To validate the paper's numerical methods, the grid-convergence and aerodynamic characters for high-lift configuration are simulated. The comparison with the experimental data of pressure and aerodynamic force from JAXA (Japan Aerospace eXploration Agency) shows that, before reaching the stall angle, the aerodynamic coefficients of the numerical simulation and Cp distribution are highly anastomosed with the experimental data, providing a preferable simulation of the aerodynamic characters of dispersion from the variation of local configurations. The paper's numerical methods are well applicable to the typical high-lift configuration and could provide technological support for the aerodynamic design of civil plane in low-speed configuration.

Key words: high-lift configuration, numerical simulation, grid convergence, aerodynamic characteristic, pressure distribution

CLC Number:

V211.7

HONG Junwu, WANG Yuntao, LI Wei, YANG Xiaochuan. Numerical simulation of high-lift configuration from HiLiftPW-3[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(3): 122391-122391.

References

[1] SLOTNICK J, KHODADOUST A, ALONSO J, et al. CFD vision 2030 study:A path to revolutionary computational aerosciences:NASA/CR-2014-218178[R].Washington,D.C.:NASA, 2014.
[2] CHRISTOPHER L R, SUSAN X Y. Prediction of high lift:Review of present CFD capability[J]. Progress in Aerospace Sciences, 2002, 38:145-180.
[3] TINOCO E N, BOGUE D R. Progress toward CFD for full flight envelope[J]. Aeronautical Journal, 2005,109:451-460
[4] ROGERS S E, ROTH K, NASH S M. Validation of computed high-lift flows with significant wind-tunnel effect[J]. AIAA Journal, 2001, 39(10):1884-1892.
[5] RUMSEY C L, GATSKI T B, SUSAN X Y, et al. Prediction of high-lift flows using turbulent closure models:AIAA-1997-2260[R]. Reston, VA:AIAA, 1997.
[6] RUDNIK R, VON GEYR H F. The European high lift project EUROLIFT Ⅱ-objectives, approach, and structure:AIAA-2007-4296[R]. Reston, VA:AIAA, 2007.
[7] RUMSEY C L, LONG M, STUEVER R A. Summary of the first AIAA CFD high lift prediction workshop(invited):AIAA-2011-939[R]. Reston, VA:AIAA, 2011.
[8] 王运涛, 洪俊武, 孟德虹. 湍流模型对梯形翼高升力构型的影响[J]. 空气动力学学报, 2013, 31(1):52-55. WANG Y T, HONG J W, MENG D H. The influence of turbulent models to trap wing simulation[J]. Acta Aerodynamica Sinica, 2013, 31(1):52-55(in Chinese).
[9] 王运涛, 李松, 孟德虹, 等. 梯形翼高升力构型的数值模拟技术[J]. 航空学报, 2014, 35(12):3213-3221. WANG Y T, LI S, MENG D H,et al.Numerical study on simulation technology of the high lift trapezoidal wing configuration[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(12):3213-3221(in Chinese).
[10] 王运涛, 李松, 孟德虹, 等. 不同襟翼偏角梯形翼构型气动特性数值模拟[J]. 航空学报, 2015, 36(6):1823-1829. WANG Y T, LI S, MENG D H, et al. Numerical simulation of the aerodynamic characteristics of the trapezoidal wing configuration with different flap angles[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(6):1823-1829(in Chinese).
[11] 洪俊武, 王运涛, 孟德虹. 结构网格方法对高升力构型的应用研究[J]. 空气动力学学报, 2013, 31(1):75-81. HONG J W, WANG Y T, MENG D H. Numerical research of high-lift configurations by structured mesh method[J]. Acta Aerodynamica Sinica, 2013, 31(1):75-81(in Chinese).
[12] 王运涛, 孟德虹, 邓小刚. 多段翼型高精度数值模拟技术研究[J]. 空气动力学学报, 2013, 31(1):88-93. WANG Y T, MENG D H, DENG X G. High-order numerical study of complex flow over multi-element airfoil[J]. Acta Aerodynamica Sinica, 2013, 31(1):88-93(in Chinese).
[13] WANG Y T, ZHANG Y L, LI S, et al. Calibration of a γ-Re_θ transition model and its validation with high-order numerical method[J]. Chinese Journal of Aeronautics, 2015, 28(3):704-711.
[14] 李松, 王光学, 王运涛, 等. WCNS格式在梯形翼高升力构型模拟中的应用研究[J]. 空气动力学学报, 2014, 32(4):439-445. LI S, WANG G X, WANG Y T, et al. Numerical simulation of high lift trapezoidal wing configuration with WCNS scheme[J]. Acta Aerodynamica Sinica, 2014, 32(4):439-445(in Chinese).
[15] 赵轲, 高正红, 黄江涛, 等. 基于分区拼接网格技术高升力装置流场数值模拟[J]. 应用力学学报, 2012, 29(1):70-75. ZHAO K, GAO Z H, HUANG J T, et al. Numerical simulation of flow around high-lift device based on zonal patched-grid technology[J]. Chinese Journal of Applied Mechanics, 2012, 29(1):70-75(in Chinese).
[16] 李萍, 李根国, 张小柯, 等. NASA高升力TrapWing全展模型的数值模拟[J]. 力学季刊, 2012, 33(2):249-255. LI P, LI G G, ZHANG X K, et al. Numerical simulation of NASA high lift trapwing full span model[J]. Chinese Quarterly of Mechanics, 2012, 33(2):249-255(in Chinese).
[17] 颜洪, 麻蓉, 聂智军, 等. 高升力标模确认计算研究[J]. 航空计算技术, 2014, 44(1):34-44. YAN H, MA R, NIE Z J, et al. CFD validation for a high-lift model[J]. Aeronautical Computing Technique, 2014, 44(1):34-44(in Chinese).
[18] 高飞飞, 颜洪, 芦彩香. NASA Trap Wing高升力标模数值模拟研究[J]. 航空计算技术, 2015, 45(1):84-90. GAO F F, YAN H, LU C X. Numerical simulation research of NASA trap wing model[J]. Aeronautical Computing Technique, 2015, 45(1):84-90(in Chinese).
[19] 赵钟, 赫新, 张来平, 等. HyperFLOW软件数值模拟Trap Wing高升力外形[J]. 空气动力学学报, 2015, 33(5):594-602. ZHAO Z, HE X, ZHANG L P, et al. Numerical research of NASA high-lift trap wing model based on HyperFLOW[J]. Acta Astronautica Sinica, 2015, 33(5):594-602(in Chinese).
[20] CHEN J T, ZHANG Y B, ZHOU N C, et al. Numerical investigations of the high-lift configuration with MFlow solver[J]. Journal of Aircraft, 2015, 52(4):1051-1062.
[21] VAN LEER B. Towards the ultimate conservation difference scheme Ⅱ, monoticity and conservation combined in a second order scheme[J]. Journal of Computational Physics, 1974, 14:361-370.
[22] YOON S, JAMESON A. Lower-upper symmetric Gauss-Sediel method for the Euler and Navier-Stokes equation[J]. AIAA Journal,1988, 26(9):1025-1026.
[23] SPALART P R, ALLMARAS S R. A one-equation turbulence model for aerodynamic flows:AIAA-1992-0439[R]. Reston, VA:AIAA, 1992.
[24] RUMSEY C L, SLOTNICK J P. Overview and summary of the second AIAA high lift prediction workshop:AIAA-2014-0747[R]. Reston, VA:AIAA, 2014.

Numerical simulation of high-lift configuration from HiLiftPW-3

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Dazhi SUN, Xi CHEN, Weicheng BAO, Wei BIAN, Qijun ZHAO. Interferences of high-speed helicopter fuselage on aerodynamic and aeroacoustic source characteristics of propeller [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529142-529142.
[2]	Chang WANG, Long HE, Dongxia XU, Min TANG, Shuai MA, Ximing WU. Flow control drag reduction of hub on coaxial rigid rotor aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529084-529084.
[3]	Yurou DAI, Jian LI, Xiaopeng XUE, Wei RONG. Aerodynamic characteristics of supersonic disk-gap-band parachute with different reefing ways [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 128811-128811.
[4]	Jiang LAI, Zhaolin FAN, Qian WANG, Siwei DONG, Fulin TONG, Xianxu YUAN. Direct numerical simulation of hypersonic cone-flare model at angle of attack [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128610-128610.
[5]	Hongjian ZHANG, Yanxin ZHANG, Jianjun XIONG, Zhao ZHAO, Lin RAN, Xian YI. Numerical simulation of phased array ultrasonic beam propagation characteristics in ice layer [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729289-729289.
[6]	Yalu FU, Xianxu YUAN, Pengxin LIU, Ming YU. Statistical properties of thermodynamic fluctuations in compressible wall⁃bounded turbulence [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(9): 127217-127217.
[7]	Siyuan CHANG, Yao XIAO, Guangli LI, Zhongwei TIAN, Kaikai ZHANG, Kai CUI. Effect of wing dihedral and anhedral angles on hypersonic aerodynamic characteristics of high-pressure capturing wing configuration [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 127349-127349.
[8]	Lei HE, Weiqi QIAN, Kangsheng DONG, Xian YI, Congcong CHAI. Aerodynamic characteristics modeling of iced airfoil based on convolution neural networks [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 126434-126434.
[9]	Wenlong BAO, He JIA, Xiaopeng XUE, Xuejiao HUANG, Shuyi GAO, Wei RONG, Qi WANG, Zhuangzhi WU. Influence of ‘windows’ structure on inflation process of ringsail parachute [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 226936-226936.
[10]	Hongyang LIU, Chao SONG, Xiao LUO, Zhu ZHOU, Guangliang LYU. Inverse design of pressure distribution for natural laminar flow nacelle considering 3D flow effects [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 126862-126862.
[11]	Rong HAN, Wei LIU, Xiaoliang YANG. Dynamic drag reduction mechanism of self-aligned aerodisks on hypersonic aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(4): 126633-126633.
[12]	Pinpeng ZENG, Shusheng CHEN, Jinping LI, Muliang JIA, Zhenghong GAO. Numerical simulation of heat reduction on blunt-headed bodies by combined scheme of drag reduction spike and annular jets [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 128407-128407.
[13]	Fenfen XIONG, Zexian LI, Yu LIU, Tangfan XIAHOU. A review of characterization methods for parameter uncertainty in engineering design based on numerical simulation [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 28611-028611.
[14]	Yunlong ZHENG, Peiqing LIU, Qiulin QU, Jiahua DAI, Yu TIAN. Numerical investigation on motion characteristics of BWB aircraft in ditching [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(21): 528588-528588.
[15]	Xia HUANG, Fan LIU, Zhitao LIU, Jinhua WU. Correlation between numerical simulation and wind tunnel test results of soft refueling [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(20): 628447-628447.