Theses and Dissertations
Issuing Body
Mississippi State University
Advisor
Thompson, David S.
Committee Member
Janus, J. Mark
Committee Member
Tong, Xiaoling
Date of Degree
12-9-2016
Document Type
Graduate Thesis - Open Access
Major
Aerospace Engineering
Degree Name
Master of Science
College
James Worth Bagley College of Engineering
Department
Department of Aerospace Engineering
Abstract
Researchers have been developing techniques to predict inlight icing in order to determine aircraft behavior under different icing conditions. A key component of the techniques is the mesh generation strategy. Automated meshing facilitates numerical simulation of ice accretion on realistic aircraft configurations by deforming the surface and volume meshes in response to the evolving ice shape. The objective of this research is to validate an ice accretion strategy for wings, using a previously developed meshing strategy. The intent is to investigate the effect of varying numerical parameters, on the predicted ice shape. Using this framework, results are simulated for rime and glaze ice accretions on a rectangular planform wing with a constant GLC-305 airfoil section. The number of time steps is shown to have a significant effect on the ice shape, depending on the icing time and conditions. Decreasing the height smoothing parameters generally improves the ice shape accuracy.
URI
https://hdl.handle.net/11668/18861
Recommended Citation
Bassou, Rania, "Validation of a Mesh Generation Strategy for Predicting Ice Accretion on Wings" (2016). Theses and Dissertations. 4936.
https://scholarsjunction.msstate.edu/td/4936