基于NACA0030的波纹状翼型气动特性探索

张庆; 叶正寅

doi:10.13700/j.bh.1001-5965.2020.0135

基于NACA0030的波纹状翼型气动特性探索

doi: 10.13700/j.bh.1001-5965.2020.0135

张庆^{1, 2},
叶正寅^3, ,

1.
西安航空学院飞行器学院, 西安 710077
2.
南洋理工大学机械与航空工程学院, 新加坡 639798
3.
西北工业大学航空学院, 西安 710072

基金项目:

国家“863”计划 2014AA7060201

国家自然科学基金 11732013

陕西省自然科学基础研究计划 2019JM-290

详细信息

通讯作者:
叶正寅. E-mail: yezy@nwpu.edu.cn

中图分类号: V211.41⁺2
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- 文章访问数: 572
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- PDF下载量: 183
- 被引次数: 0
出版历程
- 收稿日期: 2020-04-13
- 录用日期: 2020-05-15
- 网络出版日期: 2021-06-20

Aerodynamic exploration for wavy airfoil based on NACA0030

ZHANG Qing^{1, 2},
YE Zhengyin^{3
, ,}

1.
School of Aircraft, Xi'an Aeronautical University, Xi'an 710077, China
2.
School of Mechanical & Aerospace Engineering, Nanyang Technological University, Singapore 639798, Singapore
3.
School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China

Funds:

National High-tech Research and Development Program of China 2014AA7060201

National Natural Science Foundation of China 11732013

Natural Science Basic Research Program of Shaanxi 2019JM-290

More Information

Corresponding author: YE Zhengyin. E-mail: yezy@nwpu.edu.cn

摘要

摘要:
相对于光滑翼型，波纹状翼型的气动特性呈现出一些独特现象。为了深入探索这种布局的气动特点，在前期风洞试验的基础上，以NACA0030翼型为基础，设计了一组具有不同外形特征的波纹状翼型，开展了非定常数值模拟工作，详细研究了低雷诺数（Re=12×10⁴）流动情况下波纹状外形对流场涡流结构和总体气动特性的影响规律。计算结果表明：相对于光滑翼型，波纹状翼型流动的分离流现象更明显，升力和升力线斜率有明显下降，但推迟了失速现象。波纹状翼型表面越光顺，气动特性越接近于光滑翼型。虽然波纹状翼型的压差阻力大于光滑翼型，但是波纹状外形产生的回流可以减小摩擦阻力。
- 波纹状翼型 /
- 光滑翼型 /
- 低雷诺数流动 /
- 气动特性 /
- 流场结构
Abstract:
Compared with smooth airfoil, the aerodynamic characteristics of wavy airfoil exhibit some unique features. In order to further explore the aerodynamic characteristics of the wavy configuration, based on the previous wind tunnel tests, a group of wavy airfoils with different geometric shape modified from NACA0030 were designed and then unsteady numerical simulations were carried out in details to investigate the effect of waviness on the vortical structure in the flow field and overall aerodynamic characteristics in low Reynolds number (Re=12×10⁴) region. Final results show that, compared to the smooth airfoil, the separation flow for the wavy airfoil is more obvious, and the lift and its slope decrease significantly, but the stalling is delayed. The smoother the wavy surface is, the closer the aerodynamic characteristics are to the smooth airfoil. Although the pressure drag of the wavy wing is greater than that of the smooth airfoil, the recirculation generated in the corrugation can reduce the viscous drag.
- wavy airfoil /
- smooth airfoil /
- low Reynolds number flow /
- aerodynamic characteristics /
- flow field structure

HTML全文

图 1 基于NACA0030翼型的波纹状翼型

Figure 1. Wavy airfoil based on NACA0030

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图 2 不同位置的计算网格分布

Figure 2. Computational grid distribution at different positions

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图 3 NACA0030翼型的压力系数对比

Figure 3. Comparison of pressure coefficient for NACA0030 airfoil

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图 4 不同翼型的气动特性对比

Figure 4. Comparison of aerodynamic characteristics among different airfoils

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图 5 不同迎角下翼型表面的压力系数分布对比

Figure 5. Comparison of airfoil surface pressure coefficient distribution at different angles of attack

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图 6 不同迎角下压力场及流线对比

Figure 6. Comparison of pressure field and streamlines at different angles of attack

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参考文献(20)

[1]	谢长川, 王伟建, 杨超. 充气式机翼的颤振特性分析[J]. 北京航空航天大学学报, 2011, 37(7): 833-838. https://bhxb.buaa.edu.cn/CN/Y2011/V37/I7/833 XIE C C, WANG W J, YANG C. Flutter analysis of inflatable wings[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(7): 833-838(in Chinese). https://bhxb.buaa.edu.cn/CN/Y2011/V37/I7/833
[2]	华如豪, 叶正寅. 排式充气机翼的高效气动布局研究[J]. 空气动力学学报, 2012, 30(2): 184-191. doi: 10.3969/j.issn.0258-1825.2012.02.008 HUA R H, YE Z Y. Research on effective aerodynamic configuration of row inflatable wings[J]. Acta Aerodynamica Sinica, 2012, 30(2): 184-191(in Chinese). doi: 10.3969/j.issn.0258-1825.2012.02.008
[3]	张庆, 叶正寅. 一种基于充气气囊的垂尾抖振抑制新方法研究[J]. 工程力学, 2014, 31(12): 234-240. doi: 10.6052/j.issn.1000-4750.2013.06.0564 ZHANG Q, YE Z Y. Study on a new method for suppression of vertical tail buffeting using inflatable bumps[J]. Engineering Mechanics, 2014, 31(12): 234-240(in Chinese). doi: 10.6052/j.issn.1000-4750.2013.06.0564
[4]	王伟, 王华, 贾清萍. 充气机翼承载能力和气动特性分析[J]. 航空动力学报, 2010, 25(10): 2296-2301. https://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201010024.htm WANG W, WANG H, JIA Q P. Analysis on bearing capacity and aerodynamic performance of an inflatable wing[J]. Journal of Aerospace Power, 2010, 25(10): 2296-2301(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201010024.htm
[5]	卫剑征, 谭惠丰, 王伟志, 等. 充气式再入减速器研究最新进展[J]. 宇航学报, 2013, 34(7): 881-890. doi: 10.3873/j.issn.1000-1328.2013.07.001 WEI J Z, TAN H F, WANG W Z, et al. New trends in inflatable reentry aeroshell[J]. Journal of Astronautics, 2013, 34(7): 881-890(in Chinese). doi: 10.3873/j.issn.1000-1328.2013.07.001
[6]	张庆, 叶正寅. 一种新型可控方向的再入充气罩[J]. 应用力学学报, 2013, 30(4): 504-509. https://www.cnki.com.cn/Article/CJFDTOTAL-YYLX201304008.htm ZHANG Q, YE Z Y. A new controllable inflatable shield for reentry[J]. Chinese Journal of Applied Mechanics, 2013, 30(4): 504-509(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-YYLX201304008.htm
[7]	李爽, 江秀强. 火星进入减速器技术综述与展望[J]. 航空学报, 2015, 36(2): 422-440. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201502003.htm LI S, JIANG X Q. Review and prospect of decelerator technologies for mars entry[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(2): 422-440(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201502003.htm
[8]	LI S, JIANG X. Review and prospect of guidance and control for mars atmospheric entry[J]. Progress in Aerospace Sciences, 2014, 69: 40-57. doi: 10.1016/j.paerosci.2014.04.001
[9]	张庆, 叶正寅. 排式双翼布局低雷诺数气动特性计算研究[J]. 工程力学, 2019, 36(10): 244-256. https://www.cnki.com.cn/Article/CJFDTOTAL-GCLX201910028.htm ZHANG Q, YE Z Y. Computational investigations for aerodynamic characteristic analysis of low Reynolds number doubly-tandem wing configurations[J]. Engineering Mechanics, 2019, 36(10): 244-256(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-GCLX201910028.htm
[10]	张庆, 叶正寅. 基于气动导数的类X-37B飞行器纵向稳定性分析[J]. 北京航空航天大学学报, 2020, 46(1): 77-85. doi: 10.13700/j.bh.1001-5965.2019.0188 ZHANG Q, YE Z Y. Longitudinal stability analysis for X-37B like trans-atmospheric orbital test vehicle based on aerodynamic derivatives[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(1): 77-85(in Chinese). doi: 10.13700/j.bh.1001-5965.2019.0188
[11]	吕强, 叶正寅, 李栋. 充气结构机翼的设计和试验研究[J]. 飞行力学, 2007, 25(4): 77-80. doi: 10.3969/j.issn.1002-0853.2007.04.021 LV Q, YE Z Y, LI D. Design and capability analysis of an aircraft with inflatable wing[J]. Flight Dynamics, 2007, 25(4): 77-80(in Chinese). doi: 10.3969/j.issn.1002-0853.2007.04.021
[12]	HU H, TAMAI M. Bioinspired corrugated airfoil at low Reynolds numbers[J]. Journal of Aircraft, 2008, 45(6): 2068-2077. doi: 10.2514/1.37173
[13]	MURPHY J T, HU H. An experimental study of a bio-inspired corrugated airfoil for micro air vehicle applications[J]. Experiments in Fluids, 2010, 49(2): 531-546. doi: 10.1007/s00348-010-0826-z
[14]	YOKOZEKI T, SUGIURA A, HIRANO Y. Development of variable camber morphing airfoil using corrugated structure[J]. Journal of Aircraft, 2014, 51(3): 1023-1029. doi: 10.2514/1.C032573
[15]	HORD K, LIANG Y. Numerical investigation of the aerodynamic and structural characteristics of a corrugated airfoil[J]. Journal of Aircraft, 2012, 49(3): 749-757. doi: 10.2514/1.C031135
[16]	FLINT T J, JERMY M C, NEW T H, et al. Computational study of a pitching bio-inspired corrugated airfoil[J]. International Journal of Heat and Fluid Flow, 2017, 65: 328-341. doi: 10.1016/j.ijheatfluidflow.2016.12.009
[17]	TANG H, LEI Y, LI X, et al. Numerical investigation of the aerodynamic characteristics and attitude stability of a bio-inspired corrugated airfoil for MAV or UAV applications[J]. Energies, 2019, 12(20): 4021. doi: 10.3390/en12204021
[18]	BARNES C J, VISBAL M R. Numerical exploration of the origin of aerodynamic enhancements in low-Reynolds number corrugated airfoils[J]. Physics of Fluids, 2013, 25(11): 115106. doi: 10.1063/1.4832655
[19]	HO W H, NEW T H. Unsteady numerical investigation of two different corrugated airfoils[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017, 231(13): 2423-2437. doi: 10.1177/0954410016682539
[20]	SHI X, HUANG X, ZHENG Y, et al. Effects of cambers on gliding and hovering performance of corrugated dragonfly airfoils[J]. International Journal of Numerical Methods for Heat & Fluid Flow, 2016, 26(3/4): 1092-1120. http://smartsearch.nstl.gov.cn/paper_detail.html?id=9fb28e484051e2b447ddc8f459d7d5ea