空气动力学学科发展研究
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摘要
<正>一、引言空气动力学是一门兼具基础性与应用性的学科,空气动力学的研究与发展同时具备双重任务~([1]),一是加强学科基础研究,关注流动现象、剖析流动机理;二是面向型号研制亟需,注重研究和解决型号研制中的关键技术问题并提供数据支撑。空气动力学的发展方向和技术水平,对于指明国家航空飞行器及武器装备的发展方向,解决关键技术问题,提升国家国防整体实力都具有十分重要的现实意义。
引文
[1]Li Feng.Temperature oscillation and frequency of a capillary driven heat pipe with reservoir[J].International Journal of Engineering,Science and Innovative Technology,2014(7).
[2]Ai Bangcheng.The application of leading thermal protection technique on hypersonic vehicle sharp leading edge.Sino Italian Conference on Space Aerothermodynamics and Hot Structure,2000.
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[5]Sun M.Insect flight dynamics:Stability and control[J].Reviews of Modern Physics,2014,86(2):615-646.
[6]冯立好,王晋军,Choi K S.等离子体环量控制翼型增升的实验研究[J].力学学报,2013,45(6):815-821.
[7]徐思文,邓学蓥,王延奎.攻角拉起时前体非对称涡诱导摇滚运动[J].北京航空航天大学学报,2015,DOI:10.13700/j.bh.1001-5965.2014.0707.
[8]李伟,马宝峰.一种改进的松耦合方法在机翼摇滚计算中的应用[J].航空学报,2014.DOI:1035271S1000L-6893.2014.0291.
[9]杨昆淼,张卫民,王斌.基于机翼气动设计准则的超临界机翼气动优化设计[J].航空学报,2013(4).
[10]陈大斌.气动噪声风洞试验技术发展概述[J].实验流体力学,2013(2).
[11]Ma K Y,Chirarattananon P,Fuller SB,et al.Controlled flight of a biologically inspired,insect-scale robot[J].Science,2013,340(6132):603-607.
[12]Walker SM,Thomas A LR,Taylor G K.Defonnable wing kinematics in free-flying hoverflies[J].Journal of the Royal Society Interface,2010,7(42):131-142.
[13]Cheng B,Deng X,Hedrick T L.The mechanics and control of pitching manoeuvres in a freely flying hawkmoth(Manduca sexta)[J].Journal of Experimental Biology,2011,214:4092-4106.
[14]吴云,李应红.等离子体流动控制研究进展与展望[J].航空学报,2015,36(2):381-405.
[15]William J G.AFRLF-22 Dynamic Wind Tunnel Test Result[R].AIAA-99-4015,1999.
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[17]张彦仲.大飞机气动总体技术的发展[J].中国工程科学,2009,11(5):4-17.
[18]阎超,席柯,袁武,等.DPW系列会议述评与思考[J].力学进展,2011,41(6):776-784.
[19]Slotnick J,Khodadoust A,Alonso J,et al.CFD Vision 2030 Study:A Path to Revolutionary Computational Aerosciences.NASA/CR-2014-218178,2014.
[20]张来平,贺立新,刘伟,等.基于非结构,混合网格的高阶精度格式研究进展.力学进展。2013,43(2):202-236.
[21]Ekaterinaris J A.High-order accurate,low numerical diffusion methods for aerodynamics.Progress in Aerospace Sciences,2005,41:192-300.
[22]Wang Z J.High-order methods for the Euler and Navier-Stokes equations on unstructured grids.Progress in Aerospace Sciences,2007,43:1-41.
[23]Levy D W,Zickuhr T,Vassberg J C,et al.Summary of data from the first AIAA CFD drag prediction workshop[R].AIAA2002-0841.Reston:AIAA,2002.
[24]Laflin K R,Klausmeyer S M,Zickuhr T,etal.Data summary from the second AIAA computational fluid dynamics drag prediction workshop[J].AIAA Journal of Aircraft,2005,42:1165-1178.
[25]Vassberg J C,Tinoco E N,Mani M,et al.Abridged Summary of the third AIAA CFD drag prediction workshop[J].AIAA Journal of Aircraft,2008,45:781-798.
[26]Vassberg J C,Tinoco E N,Mani M,et al.Summary of the fourth AIAA CFD drag prediction workshop[R].AIAA 2010-4547.Reston:AIAA,2010.
[27]Levy D W,Laflin K R,Tinoco E N,et al.Summary of data from the fifth AIAA CFD drag prediction workshop[R].AIAA 2013-0046.Reston:AIAA,2013.
[28]Rudnik R.CFD assessment for high lift flows in the European project EUROLIFT[R].AIAA 2003-3794.Reston:AIAA,2003.
[29]Rudnik R,Von Geyr H Frhr.The European high lift project EUROLIFT II-objectives,approach,and structure[R].AIAA 2007-4296.Reston:AIAA,2007.
[30]SlotnickJP,HannonJA,Chaffin M.Overview of the First AIAA CFD High Lift Prediction Workshop(invited)[R].AIAA 2011-862.Reston:AIAA,2011.
[31]Rumsey C L,Long M,Stuever R A.Summary of the first AIAA CFD high lift prediction workshop(invited)[R].AIAA 2011-939.Reston:AIAA,2011.
(1)杨文:双自由度大幅振荡一期试验报告,2013年10月。
(2)眭建军:FL-8风洞旋转流场下大幅振荡试验报告,2013年9月。
(1)陈昊:FL-8风洞旋转流场下动导数试验报告,2013年11月。
(1)韩慧伶,王红岩,王新阁,等.大迎角空气动力性能分析[R].吉林省第七届科学技术学术年会,2012.
(1)李斌,杨智春.大型运输机水上迫降研究进展[R].中国航空学会2007年学术年会,2007.
(1)Kato.C.Engineering applications of fully-resolved LES:present status and future perspectives.The eighth international conference on computational fluid dynamics,Chengdu,China,July 14-18,2014.
[2]Ai Bangcheng.The application of leading thermal protection technique on hypersonic vehicle sharp leading edge.Sino Italian Conference on Space Aerothermodynamics and Hot Structure,2000.
[3]李锋,杨云军,刘周,等.飞行器气动/飞行,控制一体化耦合模拟技术[J].空气动力学报,2015(2).
[4]Mou X L,Liu Y P,Sun M.Wing motion measurement and aerodynamics of hovering true hoveiflies[J].Journal of Experimental Biology,2011,214:2832-2844.
[5]Sun M.Insect flight dynamics:Stability and control[J].Reviews of Modern Physics,2014,86(2):615-646.
[6]冯立好,王晋军,Choi K S.等离子体环量控制翼型增升的实验研究[J].力学学报,2013,45(6):815-821.
[7]徐思文,邓学蓥,王延奎.攻角拉起时前体非对称涡诱导摇滚运动[J].北京航空航天大学学报,2015,DOI:10.13700/j.bh.1001-5965.2014.0707.
[8]李伟,马宝峰.一种改进的松耦合方法在机翼摇滚计算中的应用[J].航空学报,2014.DOI:1035271S1000L-6893.2014.0291.
[9]杨昆淼,张卫民,王斌.基于机翼气动设计准则的超临界机翼气动优化设计[J].航空学报,2013(4).
[10]陈大斌.气动噪声风洞试验技术发展概述[J].实验流体力学,2013(2).
[11]Ma K Y,Chirarattananon P,Fuller SB,et al.Controlled flight of a biologically inspired,insect-scale robot[J].Science,2013,340(6132):603-607.
[12]Walker SM,Thomas A LR,Taylor G K.Defonnable wing kinematics in free-flying hoverflies[J].Journal of the Royal Society Interface,2010,7(42):131-142.
[13]Cheng B,Deng X,Hedrick T L.The mechanics and control of pitching manoeuvres in a freely flying hawkmoth(Manduca sexta)[J].Journal of Experimental Biology,2011,214:4092-4106.
[14]吴云,李应红.等离子体流动控制研究进展与展望[J].航空学报,2015,36(2):381-405.
[15]William J G.AFRLF-22 Dynamic Wind Tunnel Test Result[R].AIAA-99-4015,1999.
[16]Wang Z J,Lan C E.Fuzzy Logic Modeling of Nonlinear Unsteady Aerodynamics[R].AIAA-98-4351,1998.
[17]张彦仲.大飞机气动总体技术的发展[J].中国工程科学,2009,11(5):4-17.
[18]阎超,席柯,袁武,等.DPW系列会议述评与思考[J].力学进展,2011,41(6):776-784.
[19]Slotnick J,Khodadoust A,Alonso J,et al.CFD Vision 2030 Study:A Path to Revolutionary Computational Aerosciences.NASA/CR-2014-218178,2014.
[20]张来平,贺立新,刘伟,等.基于非结构,混合网格的高阶精度格式研究进展.力学进展。2013,43(2):202-236.
[21]Ekaterinaris J A.High-order accurate,low numerical diffusion methods for aerodynamics.Progress in Aerospace Sciences,2005,41:192-300.
[22]Wang Z J.High-order methods for the Euler and Navier-Stokes equations on unstructured grids.Progress in Aerospace Sciences,2007,43:1-41.
[23]Levy D W,Zickuhr T,Vassberg J C,et al.Summary of data from the first AIAA CFD drag prediction workshop[R].AIAA2002-0841.Reston:AIAA,2002.
[24]Laflin K R,Klausmeyer S M,Zickuhr T,etal.Data summary from the second AIAA computational fluid dynamics drag prediction workshop[J].AIAA Journal of Aircraft,2005,42:1165-1178.
[25]Vassberg J C,Tinoco E N,Mani M,et al.Abridged Summary of the third AIAA CFD drag prediction workshop[J].AIAA Journal of Aircraft,2008,45:781-798.
[26]Vassberg J C,Tinoco E N,Mani M,et al.Summary of the fourth AIAA CFD drag prediction workshop[R].AIAA 2010-4547.Reston:AIAA,2010.
[27]Levy D W,Laflin K R,Tinoco E N,et al.Summary of data from the fifth AIAA CFD drag prediction workshop[R].AIAA 2013-0046.Reston:AIAA,2013.
[28]Rudnik R.CFD assessment for high lift flows in the European project EUROLIFT[R].AIAA 2003-3794.Reston:AIAA,2003.
[29]Rudnik R,Von Geyr H Frhr.The European high lift project EUROLIFT II-objectives,approach,and structure[R].AIAA 2007-4296.Reston:AIAA,2007.
[30]SlotnickJP,HannonJA,Chaffin M.Overview of the First AIAA CFD High Lift Prediction Workshop(invited)[R].AIAA 2011-862.Reston:AIAA,2011.
[31]Rumsey C L,Long M,Stuever R A.Summary of the first AIAA CFD high lift prediction workshop(invited)[R].AIAA 2011-939.Reston:AIAA,2011.
(1)杨文:双自由度大幅振荡一期试验报告,2013年10月。
(2)眭建军:FL-8风洞旋转流场下大幅振荡试验报告,2013年9月。
(1)陈昊:FL-8风洞旋转流场下动导数试验报告,2013年11月。
(1)韩慧伶,王红岩,王新阁,等.大迎角空气动力性能分析[R].吉林省第七届科学技术学术年会,2012.
(1)李斌,杨智春.大型运输机水上迫降研究进展[R].中国航空学会2007年学术年会,2007.
(1)Kato.C.Engineering applications of fully-resolved LES:present status and future perspectives.The eighth international conference on computational fluid dynamics,Chengdu,China,July 14-18,2014.
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