Peach, Brian, et al. “Uniform Design Correlations for Glaze Ice Accretion and Convective Heat Transfer from an Airfoil”. 55th AIAA Aerospace Sciences Meeting, 2017, https://doi.org/10.2514/6.2017-0666.

Genre

  • Conference Proceedings
Contributors
Author: Peach, Brian
Contributor: 55th AIAA Aerospace Sciences Meeting
Author: Naterer, Greg F.
Author: Pope, Kevin
Date Issued
2017
Place Published
Grapevine, Texas
Abstract

Ice accretion on aircraft, wind turbine, power line and other surfaces is a significant technical challenge that often degrades the system performance. At sub-zero temperatures, precipitation can impact and freeze on wind blade surfaces causing icing challenges which diminishes system performance by creating rotational imbalances, structural vibrations, and reducing financial feasibility [1-4]. FENSAP-ICE is a commercial Computational Fluid Dynamics (CFD) package that simulates the ice accretion process from water droplets in air impacting onto a surface. The simulation process is performed in a staged approach by predicting the air flow field, determining water impingement limits and concentrations, and using thermal properties to evaluate freezing rates and water runback. FENSAP-ICE can evaluate resulting changes of aerodynamic forces caused by the ice build-up and effectively predict ice accretion on

Note

Statement of responsibility:

:

:

Language

  • English
Host Title
55th AIAA Aerospace Sciences Meeting