Numerical Simulation of the Processes of Icing on Airfoils with Formation of a “Barrier” Ice

Author:

Prikhod’ko A. A.,Alekseenko S. V.

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,Condensed Matter Physics

Reference33 articles.

1. T. P. Meshcheryakova, Design of Systems of Protecting Aircraft and Helicopters [in Russian], Mashinostroenie, Moscow (1977).

2. Recommendating Instruction RTs-AP33.68.33.77, Determination of the Correspondence of an Engine to the Requirements AP-33 Concerning the Ability of Its Operation under Conditions of Icing and Ice Ingestion into the Engine [in Russian], TsIAM, Moscow (2003).

3. M. B. Bragg, Aircraft aerodynamic effects due to large-droplet ice accretions, AIAA 34th Aerospace Sciences Meeting, Reno, NV, January 15–18, AIAA Paper, No. 0932 (1996).

4. S. Dutch, Natural and Applied Sciences. http://www.uwgb.edu/dutchs/EarthSC102Notes/102Clouds.htm .

5. M. Potapczuk, Numerical analysis of a NACA 0012 airfoil with leading edge ice accretions, AIAA Paper, No. 0101 (1987).

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