Citation: | GU Hong-yu, SANG Wei-min, PANG Run, et al. Numerical Simulation of Wing Hot Air Anti-Icing and Ice Ridge Formation[J]. PHYSICS OF GASES, 2019, 4(4): 41-49. DOI: 10.19527/j.cnki.2096-1642.0768 |
[1] |
Bragg M B, Perkins W R, Sarter N B, et al. An interdisciplinary approach to inflight aircraft icing safety[R]. AIAA 1998-0095, 1998.
|
[2] |
Jones S M, Reveley M S, Evans J K, et al. Subsonic aircraft safety icing study[R]. NASA/TM-2008-215107, 2008.
|
[3] |
Papadakis M, Wong S H, Yeong H W, et al. Icing tunnel experiments with a hot air anti-icing system[R]. AIAA 2008-444, 2008.
|
[4] |
Souder R H, Sheldon D W, Ide R F, et al. NASA Glenn icing research tunnel user manual[R]. NASA TM 2003-212004, 2003.
|
[5] |
Planquart P, Vanden B G, Buchlin J M. Experimental and numerical optimization of a wing leading edge hot air anti-icing system[R]. AIAA 2005-1227, 2005.
|
[6] |
Pellissier F, Habashi W, Pueyo A. Design optimization of hot-air anti-icing systems by FENSAP-ICE[R]. AIAA 2010-1238, 2010.
|
[7] |
霍西恒, 王大伟, 李革萍, 等.某型飞机机翼防冰系统性能验证研究[J].民用飞机设计与研究, 2013(4):13-16, 45. DOI: 10.3969/j.issn.1674-9804.2013.04.004
Huo X H, Wang D W, Li G P, et al. Research of wing anti-ice system performance validation for civil aircraft[J]. Civil Aircraft Design & Research, 2013(4):13-16, 45(in Chinese). DOI: 10.3969/j.issn.1674-9804.2013.04.004
|
[8] |
Wong S H, Papadakis M, Wong J. CFD analysis of a wing with a bleed air ice protection system[R]. AIAA 2013-2935, 2013.
|
[9] |
易贤.飞机积冰的数值计算与积冰试验相似准则研究[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: China Aerodynamics Research and Development Center, 2007(in Chinese).
|
[10] |
王昆, 白俊强, 夏露, 等.飞机热气防冰系统与冰脊预测的数值模拟[J].航空动力学报, 2014, 29(11):2695-2703. http://d.old.wanfangdata.com.cn/Periodical/hkdlxb201411021
Wang K, Bai J Q, Xia L, et al. Numerical simulation of aircraft hot air anti-icing system and ice ridge predic-tion[J]. Journal of Aerospace Power, 2014, 29(11):2695-2703(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkdlxb201411021
|
[11] |
Bourgault Y, Boutanios Z, Habashi W G. Three-dimensional Eulerian approach to droplet impingement simula-tion using FENSAP-ICE, Part 1:model, algorithm, and validation[J]. Journal of Aircraft, 2000, 37(1):95-103. DOI: 10.2514/2.2566
|
[12] |
胡剑平, 刘振侠, 张丽芬.霜状冰结冰数值模拟研究[J].航空计算技术, 2011, 41(6):8-11. DOI: 10.3969/j.issn.1671-654X.2011.06.003
Hu J P, Liu Z X, Zhang L F. Numerical simulation of 3D rime ice[J].Aeronautical Computing Technique, 2011, 41(6):8-11(in Chinese). DOI: 10.3969/j.issn.1671-654X.2011.06.003
|
[13] |
Bourgault Y, Beaugendre H, Habashi W. Development of a shallow-water icing model in FENSAP-ICE[J]. Journal of Aircraft, 2000, 37(4):604-646. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=1e1cb8b96ca897580a5758804c6a1c0d
|
[14] |
Saeed F, Paraschivoiu I. Optimization of a hot-air anti-icing system[R]. AIAA 2003-733, 2003.
|
[15] |
Planquart P, Vanden B G, Buchlin J M. Experimental and numerical optimization of a wing leading edge hot air anti-icing system[R]. AIAA 2005-1277, 2005.
|
[16] |
Papadakis M, Wong S H, Yeong H W, et al. Icing tunnel experiments with a hot air anti-icing system[R]. AIAA 2008-444, 2008.
|
[17] |
De Santos L C, Domingos R H, Maria R B, et al. Sensitivity analysis of a bleed air anti-ice thermal model to geometrical and operational parameters[R]. AIAA 2008-0445, 2008.
|