Abstract
This paper presents a code to simulate rime and glaze ice accretion. A Shear Stress Transport (SST) \( k - \omega \) model with roughness extension is developed to directly calculate the convective heat transfer coefficient. The airflow field is solved based on Reynolds-averaged Navier-Stokes (RANS) equations and the roughness extension of SST k–\( \omega \) model. The droplet flow field is solved based on Eulerian method. Ice accretion model based on Stefan problem was solved to simulate the film flow on the icing surface. This roughness extension model is applied to predict the skin friction coefficient and Stanton number of the MSU plate. The results are in good agreement with the experimental data. Furthermore, rime and glaze ice accretion simulations over NACA0012 airfoil are accomplished. Results show that the ice shapes of both rime ice and glaze ice agree well with the result of the IRT experiments.
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Liu, T., Cai, J., Qu, K. (2019). Ice Accretion Simulation Based on Roughness Extension of Shear Stress Transport \( \varvec{k} -\varvec{\omega} \) Turbulence Model. In: Zhang, X. (eds) The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018). APISAT 2018. Lecture Notes in Electrical Engineering, vol 459. Springer, Singapore. https://doi.org/10.1007/978-981-13-3305-7_46
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DOI: https://doi.org/10.1007/978-981-13-3305-7_46
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