[1] THOMAS S K,CASSONI R P,MACARTHUR C D.Aircraft anti-icing and de-icing techniques and modeling[J].Journal of Aircraft,1996,33(5):841-854. [2] 裘燮刚,韩凤华.飞机防冰系统[M].北京:国防工业出版社,2004.QIU X G,HAN F H.Anti-icing systems of aircraft[M].Beijing:National Defense Industry Press,2004(in Chinese). [3] 朱春玲,朱程香.飞机结冰及其防护[M].北京:科学出版社,2016.ZHU C L,ZHU C X.Aircraft icing and its protection[M].Beijing:Science Press,2016(in Chinese). [4] 林贵平,卜雪琴,申晓斌,等.飞机结冰与防冰技术[M].北京:北京航空航天大学出版社,2016.LIN G P,BU X Q,SHEN X B,et al.Aircraft icing and anti-icing/deicing technologies[M].Beijing:Beihang University Press,2016(in Chinese). [5] 任鹏飞,徐宇,宋娟娟,等.霜冰条件对翼型气动性能影响数值研究[J].工程热物理学报,2014,35(4):663-668.REN P F,XU Y,SONG J J,et al.Numerical study about the influence of rime ice conditions on airfoil[J].Journal of Engineering Thermophysics,2014,35(4):663-668(in Chinese). [6] CAO Y,HUANG J,XU Z,et al.Insight into rime ice accretion on an aircraft wing and corresponding effects on aerodynamic performance[J].The Aeronautical Journal,2016,120(1229):1101-1122. [7] BRAGG M B,BROEREN A P,BLUMENTHAL L A.Iced-airfoil aerodynamics[J].Progress in Aerospace Sciences,2005,41(5):323-362. [8] POURYOUSSEFI S G,MIRZAEI M,NAZEMI M M,et al.Experimental study of ice accretion effects on aerodynamic performance of an NACA 23012 airfoil[J].Chinese Journal of Aeronautics,2016,29(3):585-595. [9] 李国知,曹义华.旋翼结冰对直升机飞行动力学特性的影响[J].航空学报,2011,32(2):187-194.LI G Z,CAO Y H.Effects of rotor icing on helicopterflight dynamic characteristics[J].Acta Aeronautica et Astronautica Sinica,2011,32(2):187-194(in Chinese). [10] 张恒,李杰,龚志斌.多段翼型缝翼前缘结冰大迎角分离流动数值模拟[J].航空学报,2017,38(2):520733.ZHANG H,LI J,GONG Z B.Numerical simulation of separated flow around a multi-element airfoil at high angle of attack with iced slat[J].Acta Aeronautica et Astronautica Sinica,2017,38(2):520733(in Chinese). [11] 周莉,徐浩军,龚胜科,等.飞机结冰特性及防除冰技术研究[J].中国安全科学学报,2010,20(6):105-110.ZHOU L,XU H J,GONG S K,et al.Research of aircraft icing characteristics and anti-icng and deicing technology[J].China Safty Science Journal,2010,20(6):105-110(in Chinese). [12] BEAUGENDRE H,MORENCY F,HABASHI W G.FENSAP-ICE's three-dimensional in-flight ice accretion module:ICE3D[J].Journal of Aircraft,2003,40(2):239-247. [13] IULIANO E,MINGIONE G,PETROSINO F,et al.Eulerian modeling of large droplet physics toward realistic aircraft icing simulation[J].Journal of Aircraft,2011,48(5):1621-1632. [14] JUNG S K,SHIN S,MYONG R S,et al.An efficient CFD-based method for aircraft icing simulation using a reduced order model[J].Journal of Mechanical Science and Technology,2011,25(3):703-711. [15] PETROSINO F,MINGIONE G,CAROZZA A,et al.Ice accretion model on multi-element airfoil[J].Journal of Aircraft,2011,48(6):1913-1920. [16] 易贤.飞机积冰的数值计算与积冰实验相似准则研究[D].绵阳:中国空气动力研究与发展中心,2007.YI X.Numerical computation of aircraft icing and study on icing test scaling law[D].Mianyang:Chinese Aerodynamic Research and Development Center,2007(in Chinese). [17] 雷梦龙,常士楠,杨波.基于Myers模型的三维结冰数值仿真[J].航空学报,2018,39(9):21952.LEI M L,CHANG S N,YANG B.Three-dimensional numerical simulation of icing using Myers model[J].Acta Aeronautica et Astronautica Sinica,2018,39(9):21952(in Chinese). [18] 常士楠,苏新明,邱义芬.三维机翼结冰模拟[J].航空学报,2011,32(2):212-222.CHANG S N,SU X M,QIU Y F.Ice accretion simulation on three dimensional wings[J].Acta Aeronautica et Astronautica Sinica,2011,32(2):212-222(in Chinese). [19] HUANG X,MYERS B,D'AVIRRO J,et al.Icing wind-tunnel icing test on a contaminated full-scale Wing-Model at takeoff conditions:AIAA-2008-6417[R].Reston:AIAA,2008. [20] 战培国.结冰风洞研究综述[J].实验流体力学,2007,21(3):92-96.ZHAN P G.A review of icing wind tunnel[J].Journal of Experiments in Fluid Mechanics,2007,21(3):92-96(in Chinese). [21] 李周复.风洞特种实验技术[M].北京:航空工业出版社,2010.LI Z F.Techniques in special wind tunnel tests[M].Beijing:Aviation Industry Press,2010. [22] 李周复.风洞试验手册[M].北京:航空工业出版社,2015.LI Z F.Handbook of wind tunnel test[M].Beijing:Aviation Industry Press,2015(in Chinese). [23] 赵凯华.定性与半定量物理学[M].北京:高等教育出版社,2008.ZHAO K H.Qualitative and semi-quantitative physics[M].Beijing:Higher Education Press,2008(in Chinese). [24] 李之光.相似与模化[M].北京:国防工业出版社,1982.LI Z G.Similarity and modeling[M].Beijing:National Defense Industry Press,1982(in Chinese). [25] ANDERSON D N.Manual of scaling method:NASA/CR-2004-212875[R].Washington,D.C.:NASA,2004. [26] 易贤,周志宏,杜雁霞,等.考虑相变时间效应的结冰实验相似参数[J].实验流体力学,2016,30(2):14-19.YI X,ZHOU Z H,DU Y X,et al.An icing scaling parameter with the effects of phase change time[J].Journal of Experiments in Fluid Mechanics,2016,30(2):14-19(in Chinese). [27] 周志宏,易贤,桂业伟,等.考虑水滴动力学效应的结冰实验相似准则[J].实验流体力学,2016,30(2):20-25.ZHOU Z H,YI X,GUI Y W,et al.Icing scaling law with the dynamics effects of water droplets[J]Journal of Experiments in Fluid Mechanics,2016,30(2):20-25(in Chinese). [28] 李静.发动机进口静止/旋转部件结冰及结冰实验的相似研究[D].西安:西北工业大学,2015.LI J.Numerical simulation of ice accretion and study for icing scaling law on aero-engine entry components[D].Xi'an:Northwestern Polytechnical University,2015(in Chinese). [29] 张丽芬,张美华,吴丁毅,等.旋转帽罩结冰相似准则的研究[J].推进技术,2015,36(8):1164-1169.ZHANG L F,ZHANG M H,WU D Y,et al.Research on icing scaling law for rotating cone[J].Journal of Propulsion Technology,2015,36(8):1164-1169(in Chinese). [30] BILANIN,A J.Proposed modifications to ice accretion/icing scaling theory[J].Journal of Aircraft,1991,28(6):353-359. [31] 杨世铭,陶文铨.传热学[M].北京:高等教育出版社,2006.YANG S M,TAO W Q.Heat transfer[M].Beijing:Higher Education Press,2006(in Chinese). [32] 孔维梁.飞机异常结冰的过冷凝固机理及理论研究[D].上海:上海交通大学,2015.KONG W L.Mechanism and fundamental theory of supercooled water solidification on the abnormal aircraft icing[D].Shanghai:Shanghai Jiao Tong University,2015(in Chinese). [33] WRIGHT W B,RUTKOWSKI A.Validation results for LEWICE 2.0:NASA/CR-1999-208690[R].Washington,D.C.:NASA,1999. |