Improved Ice Accretion Prediction Code

Authors

  • B. Hoření Academy of Sciences of the Czech Republic
  • V. Horák University of Defence, Brno, Czech Republic
  • Z. Chára Academy of Sciences of the Czech Republic

Keywords:

aircraft icing, ice accretion simulation, icing code

Abstract

The paper deals with the further development of the computational wing airfoil ice accretion prediction code ICE. Presented version enables computational rime ice and glaze ice accretion prediction on single and multi-element airfoils in acceptable time of solution. Mathematical model has been modified for variable wall temperature along the airfoil surface. The code was also improved for the better approximation of transition boundary layer location. There are shown results ice accretion prediction of the wing airfoil with a slotted flap and various cases of predicted ice shapes in dependence of air temperature.

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Published

28-02-2022

How to Cite

Hoření, B., Horák, V., & Chára, Z. (2022). Improved Ice Accretion Prediction Code. Advances in Military Technology, 3(1), 44–50. Retrieved from https://aimt.cz/index.php/aimt/article/view/1674

Issue

Vol. 3 No. 1 (2008)

Section

Research Paper

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