Cloud calibration method of 3m×2m icing wind tunnel

Wang Zixu; Shen Hao; Guo Long; Guo Xiangdong; Ni Zhangsong

doi:10.11729/syltlx20170163

Volume 32 Issue 2

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Wang Zixu, Shen Hao, Guo Long, et al. 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

Citation:

Wang Zixu, Shen Hao, Guo Long, et al. 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

Citation:

Wang Zixu, Shen Hao, Guo Long, et al. 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

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Cloud calibration method of 3m×2m icing wind tunnel

doi: 10.11729/syltlx20170163

1.
State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China
2.
Shanghai Aircraft Airworthiness Certification Center of Civil Aviation Administration of China, Shanghai 200232, China

Received Date: 2017-12-13
Rev Recd Date: 2018-03-22
Publish Date: 2018-04-25

Abstract

Abstract

The cloud calibration has been carried out under SAE ARP5905 standard for 3m×2m icing wind tunnel, results of which can be used for certificating icing wind tunnel performance and supplying data proof for obtaining icing flight certification. Based on the ice accretion mechanism, the phase doppler interference principle, and the hot-wire principle, the calibration work was completed in the main test section by using the icing grid, PDI-FPDR, the icing blade, and LWC-200. Methods and procedures are summarized to increase the efficiency of calibration. Typical cloud calibration results indicate that the icing cloud uniformity is good, 60% of the main test section could remain target LWC within ±20%. The MVD maximum deviation is smaller than ±10%. The LWC stability is greater than ±20%. All the cloud parameters could meet the requirements of ARP5905, which could be used for supplying data proof of 3m×2m icing wind tunnel certification.
- icing wind tunnel,
- icing test,
- airworthiness,
- cloud parameter,
- calibration

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References(14)

References

[1]	SAE Aerospace. SAE ARP5905 Calibration and acceptance of icing wind tunnels[S]. SAE, 2003. http://www.sae.org/standards/content/arp5905/
[2]	Federal Aviation Administration. FAR Part25 Airworthiness standards: Transport category airplanes[S]. Federal Aviation Agency, 2008.
[3]	中国民用航空局. CCAR-25-R4中国民用航空规章第25部: 运输类飞机适航标准[S]. 北京: 中国民用航空局, 2011.
[4]	SAE Aerospace. SAE AIR4906 Droplet sizing instrumentation used in icing facilities[S]. SAE, 1995. https://www.sae.org/standards/content/air4906/
[5]	SAE. SAE AIR5320 Summary of icing simulation test facilities[S]. SAE, 1999. https://www.sae.org/standards/content/air5320/
[6]	SAE Aerospace. SAE AIR5624 Aircraft inflight icing terminology[S]. SAE, 2008. http://articles.sae.org/2917/
[7]	Sten L E, Ide R F. NASA glenn icing research tunnel: 2014 and 2015 cloud calibration procedures and results[R]. NASA/TM-2015-218758, 2015. https://www.sciencedirect.com/science/article/pii/S0376042118300058
[8]	Van Zante J F, Ide R F. NASA glenn icing research tunnel: 2014 cloud calibration procedure and results[R]. NASA/TM-2014-218392, 2014. doi: 10.2514/6.2012-2933
[9]	Bellucci M, Esposito B M. Calibration of the CIRA IWT in the low speed configuration[R]. AIAA-2007-1092, 2007. http://edu.wanfangdata.com.cn/Periodical/Detail/kjdb201325007
[10]	Ragni A, Esposito B. Calibration of the CIRA IWT in the high speed configuration[R]. AIAA-2005-471, 2005. http://www.academia.edu/28736885/Calibration_of_the_CIRA_IWT_in_the_High_Speed_Configuration
[11]	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.
[12]	朱春玲, 朱程香.飞机结冰及其防护[M].北京:科学出版社, 2016.
[13]	程尧, 张平涛, 郭向东, 等.机载式相位多普勒干涉仪在结冰风洞的应用[J].兵工自动化, 2017, 36(9):55-57. http://www.cqvip.com/QK/90272A/201502/664576270.html Cheng Y, Zhang P T, Guo X D, et al. Application of PDI-FPDR in icing wind tunnel[J]. Ordnance Industry Automation, 2017, 36(9):55-57. http://www.cqvip.com/QK/90272A/201502/664576270.html
[14]	赖庆仁, 郭龙, 李明, 等.结冰风洞液态水含量测量装置设计与实现[J].空气动力学学报. 2016, 24(6):750-755. http://industry.wanfangdata.com.cn/dl/Detail/Periodical?id=Periodical_kjdb200921018 Lai Q R, Guo L, Li M, et al. Design and implementation of the device for liquid water content measurement in icing wind tunnel[J]. Acta Aerodynamica Sinica, 2016, 24(6):750-755. http://industry.wanfangdata.com.cn/dl/Detail/Periodical?id=Periodical_kjdb200921018