Volume 29 Issue 3
Mar.  2014
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2014  >  29(3): 495-503
HU Ya-ping, JI Hong-hu, WANG Jian, CHEN Ning-li, CAO Guang-zhou, TONG Hui, PANG Li-gang. Experiment on effect of cone angle on ice accretion of rotating spinner[J]. Journal of Aerospace Power, 2014, 29(3): 495-503. doi: 10.13224/j.cnki.jasp.2014.03.003
Citation: HU Ya-ping, JI Hong-hu, WANG Jian, CHEN Ning-li, CAO Guang-zhou, TONG Hui, PANG Li-gang. Experiment on effect of cone angle on ice accretion of rotating spinner[J]. Journal of Aerospace Power, 2014, 29(3): 495-503. doi: 10.13224/j.cnki.jasp.2014.03.003
shu

Experiment on effect of cone angle on ice accretion of rotating spinner

doi: 10.13224/j.cnki.jasp.2014.03.003

  • 1. Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

  • 2. Commercial Aircraft Engine Company Limited, Aviation Industry Corporation of China, Shanghai 201108, China

  • Received Date: 2013-09-15
  • Publish Date: 2014-03-28
    Abstract
  • Simulated ice accretion tests on four sub-scale rotating spinner models with different cone angles were conducted in icing wind tunnel. The similarity parameters of ice accretion were derived for rotating surface. And the ice accretion test parameters for sub-scale spinner models were determined according to the matching of important similarity parameters. The ice accretion and final ice shapes were recorded by a high speed video system in the test. The test results show that the ice accreted on these four models is composed of early formed glaze ice which entirely covers the clean surface and subsequent white rime ice which grows rapidly. For the spinner model with cone angle is no larger than 74°, the rime ice appears in the form of needle or grain, which is relatively thinner. For the spinner model with cone angle larger than 80°, the rime ice is feather shaped which is thicker and could be partly shed from the icing surface. The position of shedding for the spinner model with larger cone angle moves downstream.

     

    • FullText(HTML)
  • loading
    • References(29)
  • [1]
    Anderson D N.Methods for scaling icing test conditions[R].AIAA 95-0540,1995.
    [2]
    Anderson D N.Further evaluation of traditional icing scaling methods[R].AIAA 96-0633,1996.
    [3]
    Saeed F,Selig S M,Bragg M B.A hybrid airfoil design method to simulate full-scale ice accretion throughout a given Cl-range[R].AIAA 97-0054,1997.
    [4]
    Ruff G A,Anderson D N.Quantification of ice accretions for icing scaling evaluations[R].AIAA 98-0195,1998.
    [5]
    Saeed F,Selig S M,Bragg M B.Experimental validation of the hybrid airfoil design procedure for full-scale ice accretion simulation[R].AIAA 98-0199,1998.
    [6]
    Anderson D N.Manual of scaling methods[R].NASA CR-2004-212875,2004.
    [7]
    Charpin,F,Fasso,G.Icing testing in the large Modane wind tunnel on full scale and reduced scale models[R].NASA/TM-75373,1979.
    [8]
    Jen-Ching T,Richard E K.Evaluation of scaling methods for rotorcraft icing[R].NASA/TM-2010-215801,2010.
    [9]
    Jen-Ching T,Richard E K.Further evaluation of scaling methods for rotorcraft icing[R].NASA/TM-2012-217418,2012.
    [10]
    Han Y Q,Palacios J,Schmitz S.Scaled ice accretion experiments on a rotating wind turbine blade[J].Journal of Wind Engineering and Industrial Aerodynamics,2012,109: 55-67.
    [11]
    Guffond D P.Icing and de-icing test on a 1/4 scale rotor in the ONERA SIMA Wind Tunnel[R].AIAA 86-0480,1986.
    [12]
    Robert J F,Randall K.B.Results of a sub-scale model rotor icing test[R].AIAA 91-0660,1991.
    [13]
    Randall K B,Thomas H B,Robert J F.An overview of a model rotor icing test in the NASA Lewis Icing Research Tunnel[R].AIAA 94-0716,1994.
    [14]
    Randall K B,Thomas H B.A review of ice accretion data from a model rotor icing test and comparison with theory[R].AIAA 91-0661,1991.
    [15]
    Baruzzi G,Tran P,Habashi W G,et al.FENSAP-ICE: progress towards a rotorcraft full 3-D icing simulation system[R].AIAA-2003-0024,2003.
    [16]
    Das K,Hamed A,Basu D.Ice shape prediction for turbofan rotating blades[R].AIAA-2006-0209,2006.
    [17]
    Fortin G,Perron J.Wind turbine icing and de-icing[R].AIAA-2009-0274,2009.
    [18]
    Fortin G,Perron J.Spinning rotor blade tests in icing wind tunnel[R].AIAA-2009-4260,2009.
    [19]
    Colin S B.Particle trajectory and icing analysis of the E3 turbofan engine using LEWICE3D version 3[R].NASA TM 2012-217696,2012.
    [20]
    陈维健,张大林.瘤状冰结冰过程的数值模拟[J].航空动力学报,2005,20(3):472-476. CHEN Weijian,ZHANG Dalin.Numerical simulation of glaze ice accretion process[J].Journal of Aerospace Power,2005,20(3):472-476.(in Chinese)
    [21]
    张强,曹义华,钟国.飞机机翼表面霜冰的三维数值模拟[J].航空动力学报,2010,25(6):1303-1309. ZHANG Qiang,CAO Yihua,ZHONG Guo.Three-dimensional numerical simulation of rime ice accretions on an aircraft wing[J].Journal of Aerospace Power,2010,25(6): 1303-1309.(in Chinese)
    [22]
    易贤,桂业伟,朱国林.飞机三维积冰模型及其数值求解方法[J].航空学报,2010,31(11):2152-2158. YI Xian,GUI Yewei,ZHU Guolin.Numerical method of a three-dimensional ice accretion model of aircraft[J].Acta Aeronautica et Astronautica Sinica,2010,31(11): 2152-2158.(in Chinese)
    [23]
    曹广州,吉洪湖,胡娅萍,等.模拟飞机迎风面三维积冰的数学模型[J].航空动力学报,2011,26(9):1953-1963. CAO Guangzhou,JI Honghu,HU Yaping,et al.An icing model for simulation three dimensional ice accretion on the upwind surfaces of a plane[J].Journal of Aerospace Power,2011,26(9): 1953-1963.(in Chinese)
    [24]
    常士楠,洪海华,张玉珠.结冰模拟与AEDC方法有效性的验证[J].北京航空航天大学学报,2009,35(6):692-696. CHANG Shinan,HONG Haihua,ZHANG Yuzhu.Icing simulation and evaluation of AEDC method[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(6):692-696.(in Chinese)
    [25]
    易贤,朱国林,桂业伟.一种改进的积冰试验相似准则及其评估[J].实验流体力学,2008,22(2):84-87. YI Xian,ZHU Guolin,GUI Yewei.Modification and evaluation of an icing scaling law[J].Journal of Experiments in Fluid Mechanics,2008,22(2): 84-87.(in Chinese)
    [26]
    胡娅萍.航空发动机进口部件积冰的数值模拟研究[R].南京:南京航空航天大学,2008. HU Yaping.Numerical simulation of ice accretion on aero-engine entry components[R].Nanjing: Nanjing University of Aeronautics and Astronautics,2008.(in Chinese)
    [27]
    赵秋月,董威,朱剑鋆.发动机旋转整流帽罩的水滴撞击特性分析[J].燃气涡轮试验与研究,2011,24(4):32-35. ZHAO Qiuyue,DONG Wei,ZHU Jianjun.Droplets impinging characteristic analysis of the rotating fairing of aero-engine[J].Gas Turbine Experiment and Research,2011,24(4): 32-35.(in Chinese)
    [28]
    王宗衍.冰风洞与结冰动力学[J].制冷学报,1999(4):15-17. WANG Zongyan.Icing wind tunnel and icing aerodynamics[J].Journal of Refrigeration,1999(4):15-17.(in Chinese)
    [29]
    《航空发动机设计手册》总编委会.航空发动机设计手册:第16册 空气系统及传热分析[M].北京:航空工业出版社,2001.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF(930.0KB)
    XML

    Article Metrics

    Article views (1683) PDF downloads(1018) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return