Modeling and Simulation of Aircraft on Ground Deicing Process Based on Thermal Balance

Article Preview

Abstract:

The deicing process and practical model of aircraft on ground were introduced, and the thermal consume was discussed. Deicing model of the aircraft on ground was founded based on thermal balance. The simulation results indicated that the proposed model was effective to analyze the aircraft on ground deicing process.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

355-358

Citation:

Online since:

November 2011

Authors:

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Eugene G. Hill. Overview of Federal Aviation Administration Aviation Safety Research for Aircraft Icing. AIAA 2006-81, (2006).

DOI: 10.2514/6.2006-81

Google Scholar

[2] CHANG Shi-nan, AI Su-xiao, CHEN Yu: Journal of System Simulation Vol. 20 (2008) No. 10, pp.2538-2545.

Google Scholar

[3] ZHANG Dalin, CHEN Wei: Journal of Aerospace Power Vol. 19 (2004) No. 1, pp.137-141.

Google Scholar

[4] Wang Ming-feng, Wang Li-xin, Huang Cheng-tao: Journal of Beijing University of Aeronautics and Astronautics Vol. 34 (2008) No. 5, pp.592-595.

Google Scholar

[5] DU Yan-xia, GUI Ye-wei, XIAO Chun-hua: Journal of Engineering Thermophysics Vol. 30 (2009) No. 11, p.1923-(1925).

Google Scholar

[6] Guilherme Araújo Lima da Silva: Journal of Aircraft Vol. 44 (2007) No. 2, pp.627-734.

Google Scholar

[7] S. Thomas, R. Cassoni, C. Mac Arthur: Aircraft anti-icing and deicing techniques and modeling. AIAA 1996-0396, (1996).

DOI: 10.2514/6.1996-390

Google Scholar

[8] P. R. Louchez, S. Bernardin, J.L. Laforte: Physical Properties of Aircraft De-icing and Anti-IcingFluids. AIAA 1998-0575, (1998).

DOI: 10.2514/6.1998-575

Google Scholar