| Citation: | WU Peipei, YAN Tao, MA Saiqiang. Numerical simulation of performance of engine lip electro-thermal anti-icing system[J]. Journal of Aerospace Power, 2020, 35(10): 2056-2063. doi: 10.13224/j.cnki.jasp.2020.10.005
|
| [1] |
汪涛,王俊琦,王朝蓬.直升机进气道防冰试验方法设计与试验［J］.科学技术与工程,2017,17(20):294-301. WANG Tao,WANG Junqi,WANG Zhaopeng.Method design of helicopter inlet duct anti-ice and experiment［J］.Science Technology and Engineering,2017,17(20):294-301.(in Chinese)
|
| [2] |
裘燮纲,韩凤华.飞机防冰系统［M］.北京:国防工业出版社,1985.
|
| [3] |
张书晔,徐伟,于磊.飞机发动机唇口防冰系统仿真分析［J］.飞机设计,2016,36(6):58-64. ZHANG Shuye,XU Wei,YU Lei.Emulation analysis for engine lip anti-ice system［J］.Aircraft Design,2016,36(6):58-64.(in Chinese)
|
| [4] |
KEITH T,Jr,DE WITT K J.Numerical simulation of an electrothermally de-iced aircraft surface using the finite element method［R］.AIAA 91-0268,1991.
|
| [5] |
MAHDI P,HABASHI W G.Aero-thermal optimization of in-flight electro-thermal ice protection systems in transient de-icing mode［J］.International Journal of Heat and Fluid Flow,2015,54:167-182.
|
| [6] |
BU X,YU J,LIN G,et al.Electrothermal airfoil anti-icing system simulation［J］.Hkie Transactions,2010,17(2):9-13.
|
| [7] |
钟国.翼型电热防/除冰系统的数值模拟［J］.航空制造技术,2011(4):75-79. ZHONG Guo.Simulation of airfoil electro-thermal anti-ice/de-ice system［J］.Aeronautical Manufacturing Technology,2011(4):75-79.(in Chinese)
|
| [8] |
霍西恒,屠敏,常士楠,等.CJ818客机尾翼周期电热除冰系统计算分析［J］.民用飞机设计与研究,2009(增刊1):126-130. HUO Xiheng,TU Min,CHANG Shinan,et al.Cycle electrothermal de-icing system analysis of CJ818 aircraft tail［J］.Civil Aircraft Design and Research,2009(Suppl.1):126-130.(in Chinese)
|
| [9] |
REID T,BARUZZI G S,HABASHI W G.FENSAP-ICE:unsteady conjugate heat transfer simulation of electrothermal de-icing［J］.Journal of Aircraft,2012,49(4):1101-1109.
|
| [10] |
FAKOREDE O,IBRAHIM H,ILINCA A,et al.Experimental investigation of power requirements for wind turbines electrothermal anti-icing systems［M］.Rijeka,Croatia:［s.n.］,2016.
|
| [11] |
BUSCHHORN S T,KESSLER S S,LACHMANN N,et al.Electro thermal icing protection of aerosurfaces using conductive polymer nanocomposites［R］.AIAA-2013-1729,2013.
|
| [12] |
杨诗雨,常士楠,高艳欣,等.旋转帽罩电加热防冰瞬态过程研究［J］.空气动力学学报,2016,34(3):289-294. YANG Shiyu,CHANG Shinan,GAO Yanxin,et al.Investigation of rotary cone electric heating anti-icing transient process［J］.Acta Aerodynamic Sinica,2016,34(3):289-294.(in Chinese)
|
| [13] |
董威,朱剑鋆,周志翔,等.航空发动机支板热滑油防冰性能试验［J］.航空学报,2014,35(7):1845-1853. DONG Wei,ZHU Jianyun,ZHOU Zhixiang,et al.Test on performance of an aero-engine strut hot lubrication oil anti-icing system［J］.Acta Aeronautica et Astronuatica Sinica,2014,35(7):1845-1853.(in Chinese)
|
| [14] |
朱光亚.电加热防冰部件加热功率的分布特性研究［D］.南京:南京航空航天大学,2014. ZHU Guangya.Study on heat power distribution characteristic for aircraft anti-ice components［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2014.(in Chinese)
|
| [15] |
马辉,张大林,孟繁鑫,等.复合材料部件电加热防冰性能试验［J］.航空学报,2013,34(8):1846-1853. MA Hui,ZHANG Dalin,MENG Fanxin,et al.Experimental of electro-thermal anti-icing on a composite assembly［J］.Acta Aeronautica et Astronuatica Sinica,2013,34(8):1846-1853.(in Chinese)
|
| [16] |
雷桂林,郑梅,董威,等.航空发动机进气支板电热防冰试验［J］.航空学报,2017,38(8):54-65. LEI Guilin,ZHENG Mei,DONG Wei,et al.Test on electrothermal anti-icing of aero-engine inlet strut［J］.Acta Aeronautica et Astronautica Sinica,2017,38(8):54-65.(in Chinese)
|
| [17] |
WIROGO S,SRIRAMBHATLA S.An Eulerian method to calculate the collection efficiency on two and three dimensional bodies［R］.AIAA-2003-1073,2003.
|
| [18] |
孙志国,付斌,朱春玲.探头式结冰探测器安装位置分析［J］.航空动力学报,2011,26(12):2676-2683. SUN Zhiguo,FU Bin,ZHU Chunling.Analysis on installation location of probe-style ice detectors［J］.Journal of Aerospace Power,2011,26(12):2676-2683.(in Chinese)
|
| [19] |
MINGIONE G,BRANDI V,ESPOSITO B.Ice accretion prediction on multi-element airfoils［R］.AIAA 97-0178,1997.
|
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