Gao Guochi, Ding Li, Li Baoliang, Wang Zixu, Jiang Yubiao. Airworthiness certification technology about icing wind tunnel test for pneumatic de-icing aircraft[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(2): 85-94. DOI: 10.11729/syltlx20180067
Citation: Gao Guochi, Ding Li, Li Baoliang, Wang Zixu, Jiang Yubiao. Airworthiness certification technology about icing wind tunnel test for pneumatic de-icing aircraft[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(2): 85-94. DOI: 10.11729/syltlx20180067

Airworthiness certification technology about icing wind tunnel test for pneumatic de-icing aircraft

More Information
  • Received Date: June 27, 2018
  • Revised Date: December 02, 2018
  • Civil aircraft should conduct icing airworthiness certification according to relevant icing airworthiness regulation requirements, so understanding the airworthiness regulations requirements and formulating the effective conformity certification process are the key points of airworthiness certification. Based on an engineering application of icing wind tunnel test for the Y12F aircraft, relative airworthiness documents, latest aircraft icing research results, certification requests and techniques are summarized, such as setting of target test cases, confirmation of facility, transformation of test cases, test model designing and manufacturing, icing wind tunnel testing and so on. The formed airworthiness certification method conducts the certification of Y12F airplane de-icing system effectively, which is accepted by Civil Aviation Administration of China (CAAC) and Federal Aviation Administration (FAA) synchronously, and it lays a good foundation for getting the aircraft certification of CAAC and FAA.
  • [1]
    Smalley C L. Certification of Part 23 airplanes for flight in icing conditions[R]. FAA: AC23. 1419-2D, 2007.
    [2]
    Potapczuk M G. Lewice E: an Euler based ice accretion code[R]. NASA-TM-105389, 1992.
    [3]
    Ruff G A, Berkowitz B M. Users manual for the NASA Lewis ice accretion prediction code (Lewice)[R]. NASA-CR-185129, 1990.
    [4]
    Brandi V, Mingione G. Ice accretion prediction on multi-element airfoils[R]. AIAA-1997-0177, 1997.
    [5]
    Croce G, Beaugendre H, Habashi W G. CHT3D: FENSAP-ICE conjugate heat transfer computations with droplet impingement and runback effects[R]. AIAA-2002-0386, 2002.
    [6]
    Bartlett C S. An empirical look at tolerances in setting icing test conditions with particular application to icing similitude[R]. DOT/FAA/CT-87/31 and AEDC-TR-87-23, 1988.
    [7]
    Bragg M, Broeren A, Addy H, et al. Airfoil ice-accretion aerodynamics simulation[R]. AIAA-2007-85, 2007.
    [8]
    Cabler S J M. Aircraft ice protection[R]. FAA: AC20-73A, 2006.
    [9]
    中国民用航空局.航空器型号合格审定程序: AP-21-AA-2011-03-R4[S].北京: 中国民用航空局航空器适航审定司, 2011.
    [10]
    Jones A R, Lewis W. Recommended values of meteorological factors to be considered in the design of aircraft ice-prevention equipment[R]. NACA-TN-1855, 1949.
    [11]
    Hacker P T, Dorsch R G. A summary of meteorological conditions associated with aircraft icing and a proposed method of selecting design criterions for ice-protection equipment[R]. NACA-TN-2569, 1951.
    [12]
    Lewis W, Bergrun N R. A probability analysis of the meteorological factors conductive to aircraft icing in the United States[R]. NACA-TN-2738, 1952.
    [13]
    Gent R W, Dart N P, Cansdale J T. Aircraft icing[J]. Phil Trans R Soc Lon A, 2000, 358:2873-2911. DOI: 10.1098/rsta.2000.0689
    [14]
    中国民用航空局.运输类飞机适航标准: CCAR-25-R4[S].北京: 中国民用航空局政策法规司, 2011.
    [15]
    Pellicano Paul. Supercooled large droplet (SLD) icing and certification of Part 23 airplanes[C]//Proc of the FAA 2009 Small Airplane Directorate Program Managers Meeting. 2009.
    [16]
    Broeren A P, Bragg M B. Effect of residual and intercycle ice accretions on airfoil performance[R]. DOT/FAA/AR-02/68, 2002.
    [17]
    Pellicano P. Residual and inter-cycle ice for lower-speed aircraft with pneumatic boots[R]. AIAA-2007-1090, 2007.
    [18]
    Rios M, Riley J T, Dumont C J. A study of intercycle, residual, and preactivation ice accretion[R]. AIAA-2001-0089, 2001.
    [19]
    Broeren A P, Bragg M B, Addy H E. Effect of intercycle ice accretions on airfoil performance[J]. Journal of Aircraft, 2004, 41(1):165-174. DOI: 10.2514/1.1683
    [20]
    Addy H E, Potatpczuk M G, Sheldon D W. Modern airfoil ice accretions[R]. AIAA-97-0174, 1997.
    [21]
    Bragg M B, Broeren A P, Blumenthal L A. Iced-airfoil aero-dynamics[J]. Progress in Aerospace Sciences, 2005, 41:323-362. DOI: 10.1016/j.paerosci.2005.07.001
    [22]
    Broeren A, Bragg M B. Effect of airfoil geometry on performance with simulated intercycle ice accretions[J]. Journal of Aircraft, 2005, 42(1):121-130. DOI: 10.2514/1.4734
    [23]
    Sae Society of Automotive Engineers. Calibration and acceptance of icing wind tunnels: SAE ARP 5905-2003[S]. AC-9C Aircraft Icing Technology Committee, 2003.
    [24]
    Pellicano Paul. Guidance for new airplane icing certification projects[C]//Proc of the SAE 2007 Aircraft & Engine Icing International Conference. 2007.
    [25]
    Kind R J. Scaling of icing tests:a review of recent progress[J]. AIAA Journal, 2003, 41(8):1421-1428. DOI: 10.2514/2.2120
    [26]
    Anderson D N. Rime-, mixed-and glaze-ice evaluations of three scaling laws[R]. AIAA-94-0718, 1994.
    [27]
    Anderson D N. Manual of scaling methods[R]. NASA/CR-2004-212875, 2004.
    [28]
    中国民用航空局.正常类、实用类、特技类和通勤类飞机适航规定: CCAR-23-R3[S].北京: 中国民用航空局飞行标准司, 2005.
  • Related Articles

    [1]ZHU Dongyu, FENG Qiang, Han Xiaotao, Yang Ximing, Cui Xiaochun, Yuan Li. Researches on a large natural moveable icing wind tunnel and test methods[J]. Journal of Experiments in Fluid Mechanics, 2022, 36(1): 52-61. DOI: 10.11729/syltlx20210100
    [2]GUO Xiangdong, ZHANG Pingtao, ZHAO Xianli, YANG Shengke, LIN Wei. The compliance verification of thermodynamic flowfield in the large icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(5): 79-88. DOI: 10.11729/syltlx20190113
    [3]ZHU Xinxin, LONG Yongsheng, SHI Youan, YANG Qingtao, ZHOU Ping, ZHAO Shunhong. Optimal design of steady enthalpy probe and test verification[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(4): 87-93. DOI: 10.11729/syltlx20190062
    [4]Zhang Hui, Fan Litao. Correlation analysis of large low speed wind tunnel test on CHN-T1 calibration model[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(3): 106-111. DOI: 10.11729/syltlx20180046
    [5]Gao Guochi, Li Baoliang, Ding Li, Wang Zixu, Ni Zhangsong. Icing wind tunnel test technology for pneumatic de-icing aircraft[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(2): 95-101. DOI: 10.11729/syltlx20180064
    [6]Wang Zixu, Shen Hao, Guo Long, Guo Xiangdong, Ni Zhangsong. Cloud calibration method of 3m×2m icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(2): 61-67. DOI: 10.11729/syltlx20170163
    [7]Zhou Feng, Feng Lijuan, Xu Chaojun, Zhao Keliang, Han Zhirong. Determination and verification of critical ice shape for the certification of civil aircraft[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(2): 8-13. DOI: 10.11729/syltlx20160019
    [8]Shen Chen, Yang Zhigang. Numerical methods exploration and experimental validation of Ahmed model with consideration of fluid-solid-interaction effect[J]. Journal of Experiments in Fluid Mechanics, 2014, (4): 37-42. DOI: 10.11729/syltlx20130017
    [9]YUAN Hong-gang, YANG Yong-dong, ZHANG Gui-chuan, HUANG Ming-qi. Improving techniques and validating of rotor and fuselage compound model test stand[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(4): 87-90. DOI: 10.3969/j.issn.1672-9897.2012.04.018
    [10]GUO Shan-guang, LIU Jun, JIN Liang, LUO Shi-bin. Numerical simulation and experiment validation on shock oscillations of inner flow path of hypersonic vehicle[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(1): 7-11. DOI: 10.3969/j.issn.1672-9897.2012.01.002
  • Cited by

    Periodical cited type(0)

    Other cited types(3)

Catalog

    Article Metrics

    Article views (368) PDF downloads (25) Cited by(3)
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return
    x Close Forever Close