基于OpenFOAM的水陆两栖飞机水面高速滑行研究

doi:10.7527/S1000-6893.2018.22330

流体力学与飞行力学

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

基于OpenFOAM的水陆两栖飞机水面高速滑行研究

段旭鹏¹, 孙卫平², 魏猛², 杨永¹

1. 西北工业大学航空学院, 西安 710072;
2. 中航通用飞机有限责任公司, 珠海 519040

收稿日期:2018-05-15 修回日期:2018-06-14 出版日期:2019-01-15 发布日期:2018-07-13
通讯作者: 杨永 E-mail:yyang@nwpu.edu.cn

Numerical simulation of amphibious aircraft taxiing at high speed on water using OpenFOAM

DUAN Xupeng¹, SUN Weiping², WEI Meng², YANG Yong¹

1. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. China Aviation Industry General Aircraft Institute Co., Ltd., Zhuhai 519040, China

Received:2018-05-15 Revised:2018-06-14 Online:2019-01-15 Published:2018-07-13

摘要/Abstract

摘要： 在开源软件OpenFOAM的两相流动态解算器中添加了激励盘，数值研究了考虑动力影响的大型四发涡桨水陆两栖飞机在水面高速滑行时的典型力学特性。针对水陆两栖飞机的特殊性，全面考虑了飞机高速滑行时的水动力、气动力、地面效应以及螺旋桨的动力影响，较为真实地模拟了飞行器水上起飞的瞬时状态。首先，在interDyMFoam中添加了激励盘模型，以体积力的形式将螺旋桨旋转产生的动量注入流场，用以模拟飞机起飞时大拉力情况下滑流的动力学影响，较螺旋桨非定常模拟方法大幅减少了计算量。其次，对Wigley船体标模和螺旋桨单桨模型分别进行了考核，验证了OpenFOAM的水动力计算能力并确认了新加入的动态激励盘方法的可靠性。最后，利用建立的方法研究了水陆两栖飞机水面单断阶滑行过程中的气动力和水动力特性并给出了滑流和动力的影响规律。

关键词: OpenFOAM, 两相流, 激励盘, 水陆两栖飞机, 滑流

Abstract: An actuator disk method is coupled with the dynamic two-phase flow solver in OpenFOAM. A numerical study is conducted for the dynamic characteristics of an amphibious aircraft with four turboprop engines during taxiing at high speed on water. Considering the particularity of amphibious aircraft, the effects of hydrodynamics, aerodynamics, slipstream of propellers together with the ground effect of water are studied simultaneously by simulating the instantaneous state when the aircraft is about to leave water. Firstly, to simulate the slipstream of propellers during takeoff, an actuator disk code is added in interDyMFoam solver, which greatly improves the efficiency of computation compared with the direct simulation of propeller rotation.The momentum generated by the rotation of the propeller is injected into the flow field in the form of volume force to simulate the dynamic effect of the slipstream of the large thrust during the aircraft takeoff process. Secondly, both the hydrodynamic calculation ability of OpenFOAM and the newly added actuator disk are validated through the Wigley model of towing tank test and the single propeller wind tunnel test. At last, the characteristics of hydrodynamics and aerodynamics of amphibious aircraft taxiing at high speed on water are analyzed by the coupled solver and the thrust of power combined with slipstream effect is investigated as well.

Key words: OpenFOAM, two-phase flow, actuator disk, amphibious aircraft, slipstream

中图分类号:

段旭鹏, 孙卫平, 魏猛, 杨永. 基于OpenFOAM的水陆两栖飞机水面高速滑行研究[J]. 航空学报, 2019, 40(1): 522330-522330.

DUAN Xupeng, SUN Weiping, WEI Meng, YANG Yong. Numerical simulation of amphibious aircraft taxiing at high speed on water using OpenFOAM[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(1): 522330-522330.

参考文献

[1] REMINGTON W. The Canadair CL-215 amphibious aircraft-Development and applications:AIAA-1989-1541[R]. Reston, VA:AIAA, 1989.
[2] LARSSON L, STERN F, BERTRAM V. Benchmarking of computational fluid dynamics for ship flows:The Gothenburg 2000 workshop[J]. Journal of Ship Research, 2003, 47(1):63-81.
[3] MAVRIPLIS D J, VASSBERG J C, TINOCO E N, et al. Grid quality and resolution issues from the drag prediction workshop series[J]. Journal of Aircraft, 2009, 46(3):935-950.
[4] QIU L J, SONG W B. Efficient decoupled hydrodynamic and aerodynamic analysis of amphibious aircraft water takeoff process[J]. Journal of Aircraft, 2013, 50(5):1369-1379.
[5] QU Q L, LIU C S, LIU P Q. Numerical simulation of water-landing performance of a regional aircraft[J]. Journal of Aircraft, 2016, 53(6):1680-1689.
[6] RANKINE W J M. On the mechanical principles of the action of propellers[J]. Transactions of the Institution of Naval Architects, 1865, 6:13-39.
[7] FROUDE R E. On the part played in propulsion by differences of fluid pressure[J]. Transactions of the Institution of Naval Architects, 1889, 30:390-423.
[8] FROUDE W. On the elementary relation between pitch, slip, and propulsive efficiency:NASA-TM-X-61726[R]. Washington, D.C.:NASA, 1920.
[9] GLAUERT H. Airplane propellers[M]. Berlin:Springer, 1935:169-360.
[10] MARQUEZ G C, STUERMER A, CLEMEN C, et al. Validation of actuator disk simulations of CROR propulsion systems at low-speed flight conditions:AIAA-2012-2787[R]. Reston, VA:AIAA, 2012.
[11] 夏贞锋, 罗淞, 杨永. 基于激励盘理论的螺旋桨滑流数值模拟研究[J]. 空气动力学学报, 2012, 30(2):219-222. XIA Z F, LUO S, YANG Y. Numerical simulations of propeller slipstream flows using actuator disk theory[J]. Acta Aerodynamica Sinica, 2012, 30(2):219-222(in Chinese).
[12] GREENSHIELDS C J. OpenFOAM user guide, version 4.0[M]. London:OpenFOAM Foundation Ltd., 2015.
[13] ISSA R I. Solution of the implicitly discretised fluid flow equations by operator-splitting[J]. Journal of Computational Physics, 1986, 62(1):40-65.
[14] RHIE C M, CHOW W L. Numerical study of the turbulent flow past an airfoil with trailing edge separation[J]. AIAA Journal, 1983, 21(11):1525-1532.
[15] KARRGOLM F P. Rhie-Chow interpolation in OpenFOAM[R/OL].(2006-5-22)[2018-03-14]. http://www.tfd.chalmers.se/~hani/kurser/OS_CFD_2007/rhiechow.pdf.
[16] BARRON R M, SALEHI N A. Effects of under? relaxation factors on turbulent flow simulations[J]. International Journal for Numerical Methods in Fluids, 2003, 42(8):923-928.
[17] MENTER F R, CARREGAL F J, ESCH T, et al. The SST turbulence model with improved wall treatment for heat transfer predictions in gas turbines[C]//Proceedings of the International Gas Turbine Congress, 2003.
[18] JASAK H, TUKOVIĆ Z. Automatic mesh motion for the unstructured finite volume method[J]. Transactions of FAMENA, 2006, 30(2):1-20.
[19] SVENNING E. Implementation of an actuator disk in OpenFOAM[R/OL]. (2010-10-30)[2018-03-14].http://www.tfd.chalmers.se/~hani/kurser/OS_CFD_2010/erikSvenning/erikSvenningReport.pdf.
[20] GOLDSTEIN S. On the vortex theory of screw propellers[J]. Proceedings of the Royal Society of London Series A, 1929, 123(792):440-465.
[21] SHOEMAKER J M, BELL J W. Complete tank tests of two flying-boat hulls with pointed steps:NACA-TN-504[R]. Washington, D.C.:NACA, 1934.
[22] 李博, 梁德旺, 黄国平. 基于等效盘模型的滑流对涡桨飞机气动性能的影响[J]. 航空学报, 2008, 29(4):845-852. LI B, LIANG D W, HUANG G P. Propeller slipstream effects on aerodynamic performance of turboprop airplane based on equivalent actuator disk model[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(4):845-852(in Chinese).
[23] 胡国才, 刘嘉, 孙建国. 螺旋桨飞机近地飞行时的纵向稳定性[J]. 海军航空工程学院学报, 2009, 24(6):601-604. HU G C, LIU J, SUN J G. Longitudinal stability of propeller aircraft during low altitude flight[J]. Journal of Naval Aeronautical and Astronautical University, 2009, 24(6):601-604(in Chinese).
[24] 孙华伟. 滑行面形状对滑行艇阻力与航态影响数值分析[D]. 哈尔滨:哈尔滨工程大学, 2012:1-50. SUN H W. Numerical analysis of planning-hull surface shape on resistance and sailing attitude[D]. Harbin:Harbin Engineering University, 2012:1-50(in Chinese).
[25] 褚林塘. 水上飞机水动力设计[M]. 北京:航空工业出版社, 2014:67-123. CHU L T. Seaplane hydrodynamic design[M]. Beijing:Aviation Industry Press, 2014:67-123(in Chinese).
[26] YANG Z, YANG W. Complex flow for wing-in-ground effect craft with power augmented ram engine in cruise[J]. Chinese Journal of Aeronautics, 2010, 23(1):1-8.

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

基于OpenFOAM的水陆两栖飞机水面高速滑行研究

Numerical simulation of amphibious aircraft taxiing at high speed on water using OpenFOAM

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	安利平, 王昊, 王掩刚, 朱自环. 跨声速压气机湿压缩性能及流动特性[J]. 航空学报, 2022, 43(9): 126024-126024.
[2]	马世赫, 李志超, 刘桂贤, 张永俊, 王瑞祥. 脉冲气体辅助掩模电解加工技术[J]. 航空学报, 2022, 43(4): 525646-525646.
[3]	叶青, 饶炜, 刘锋, 孙泽洲, 刘国强, 王闯, 董捷, 韩泉东, 缪远明, 谭志云, 陆慧林. 火星着陆发动机羽流与火壤的相互作用[J]. 航空学报, 2022, 43(3): 626557-626557.
[4]	吕亚国, 姜乐, 高晓果, 刘振侠, 朱鹏飞, 高文君. 高速轴承环下润滑收油叶片结构参数与工况参数间的匹配关系[J]. 航空学报, 2022, 43(12): 426037-426037.
[5]	饶崇, 张铁军, 魏闯, 刘影. 一种分布式电动飞机螺旋桨滑流影响机理[J]. 航空学报, 2021, 42(S1): 726387-726387.
[6]	卢昱锦, 肖天航, 邓双厚, 支豪林, 朱震浩, 陆召严. 着水初始条件对水陆两栖飞机着水性能的影响[J]. 航空学报, 2021, 42(7): 124483-124483.
[7]	童明波, 陈吉昌, 李乐, 肖天航, 古彪, 董登科, 汪正中. 飞行器水载荷结构完整性数值模拟现状与展望-Part I:水上迫降和水上漂浮[J]. 航空学报, 2021, 42(5): 524530-524530.
[8]	赵立杰, 田孟伟, 李景奎, 王明阳, 刘达. 水上电动飞机浮筒设计及起飞滑行[J]. 航空学报, 2021, 42(3): 624590-624590.
[9]	田文朋, 夏峰, 宋鹏飞, 张柁, 杨鹏飞. 水陆两栖飞机静力试验优化机翼变形的载荷配平[J]. 航空学报, 2020, 41(11): 223956-223956.
[10]	薛帅杰, 刘红军, 陈鹏飞, 夏益志. 注气离心喷嘴喷注过程稳定性试验[J]. 航空学报, 2019, 40(7): 122697-122697.
[11]	邓磊, 段卓毅, 钱瑞战, 许瑞飞, 高永卫. 螺旋桨滑流对短舱/机翼构型尾迹流场的影响[J]. 航空学报, 2019, 40(5): 122434-122434.
[12]	缪涛, 陈波, 马率, 杨小川, 丁兴志. 基于动态重叠网格方法的尾翼对螺旋桨滑流的影响[J]. 航空学报, 2019, 40(4): 622338-622338.
[13]	马率, 邱名, 王建涛, 缪涛, 江雄. CFD在螺旋桨飞机滑流影响研究中的应用[J]. 航空学报, 2019, 40(4): 622365-622365.
[14]	赵帅, 段卓毅, 李杰, 钱瑞战, 许瑞飞. 涡桨飞机螺旋桨滑流气动干扰效应及流动机理[J]. 航空学报, 2019, 40(4): 122469-122469.
[15]	陈波, 缪涛, 马率, 耿建中, 江雄. 螺旋桨飞机俯仰力矩特性改进方法[J]. 航空学报, 2019, 40(4): 622341-622341.