[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]
BALLISIIC AND AIRDYNAMICS

Numerical Simulation for Influence of Vertical Height Difference to Aerodynamic Characteristics of “Diamond Back" Wing

  • CHEN Junkui ,
  • WANG Zhijun ,
  • ZHANG Lianbo ,
  • ZHANG Juanting ,
  • WU Guodong
Expand
  • 1 School of Mechatronics Engineering, North University of China, Taiyuan 030051, China
    2 No. 93705 Unit, Hebei Tangshan 064200, China
    3 School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
    4 National Key Laboratory for Electronic Measurement Technology, North University of China, Taiyuan 030051, China

Received date: 2014-04-30

  Online published: 2025-05-26

Abstract

Based on geometry and design parameters of "diamond back" wing, influence of vertical height difference of the anterior and posterior wing aerodynamic characteristics at low Reynolds number were simulated by two-dimensional computational model which use NACA6411 airfoil. The simulation results indicate that the Transition SST turbulence model high accuracy and creditability in solving flowing around an airfoil at low Reynolds number; Near the station of leading edge distance between the anterior and posterior wing is about 1.5 times that of chord length of anterior airfoil, the influence of vertical height difference aerodynamic characteristics appear the phenomenon that change trend reversal; One of effective optimization methods for “diamond back" aerodynamic configuration is designing the vertical height difference and the leading edge distance between the tip chord of the anterior and posterior wing rationally, if these values are 22 mm and 100 mm, it both can achieve optimization and is convenient for engineering application.

Cite this article

CHEN Junkui , WANG Zhijun , ZHANG Lianbo , ZHANG Juanting , WU Guodong . Numerical Simulation for Influence of Vertical Height Difference to Aerodynamic Characteristics of “Diamond Back" Wing[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(2) : 109 -113 . DOI: 10.15892/j.cnki.djzdxb.2015.02.028

[an error occurred while processing this directive]

References

[1]
雷娟棉, 胡俊, 吴甲生. 小直径炸弹(SDB)气动力问题[J]. 弹箭与制导学报, 2004, 24(3):169-170.
[2]
雷娟棉, 吴甲生. 钻石背弹翼外形参数对气动特性的影响[J]. 北京理工大学学报, 2006, 26(11):945-948.
[3]
雷娟棉, 吴甲生. 钻石背弹翼气动特性风洞实验研究[J]. 兵工学报, 2007, 28(7):893-896.
[4]
吴小胜, 雷娟棉, 吴甲生. “钻石背”弹翼气动特性数值模拟研究[J]. 兵工学报, 2010, 31(8):1048–1052.
[5]
吴小胜. 折叠式主弹翼气动特性研究[J]. 北京理工大学学报, 2010, 30(9):1024-1027.
[6]
李锋, 白鹏, 石文, 等. 微型飞行器低雷诺数空气动力学[J]. 力学发展, 2007, 37(2):257-268.
[7]
Langtry R B, Menter F R. Transition modeling for general CFD applications in aeronautics. AIAA Paper, 2005-0522[R]. 2005.
[8]
Menter F R, Langtry R B, Likki S R, et al. Acorrelationbased transition model using local variables part I-Model formulation, GT2004-53452 [R]. 2004.
[9]
Menter F R, Langtry R B, Likki S R, et al. Acorrelationbased transition model using local variables part II-Test cases and industrial applications, GT2004-53454 [R]. 2004
[10]
刘沛清, 马利川, 屈秋林, 等. 低雷诺数下翼型层流分离泡及吹吸气控制数值研究[J]. 空气动力学学报, 2013, 31(4): 518-524.
[12]
Selig M S, Deters R W, Williamson G A. Wind tunnel testing airfoil sat Low Reynolds Numbers, AIAA 2011-875[R]. 2011.
[13]
Selig M S, McGranahan B D. Wind tunnel aerodynamic tests of six airfoils for use on small wind turbines, NREL/SR-500-34515 [R]. 2004.
[14]
文晓庆, 柳阳威, 方乐, 等. 提高k-ω SST 模型对翼型失速特性的模拟能力[J]. 北京航空航天大学学报, 2013, 39(8): 1127-1132.
[15]
Langtry R B, Gola J, Mente F R. Predicting 2D airfoil and 3Dwind turbine rotor performance using a transition model for general CFD codes, AIAA 2006-395 [R]. 2006.
[16]
SheltonA, Abras J, Jurenko R, et al. Improving the CFD predictions of airfoils install, AIAA2005-1227 [R]. 2005.
Outlines

/

[an error occurred while processing this directive]