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Discrete Surface Evolution and Mesh Deformation for Aircraft Icing ApplicationsRobust, automated mesh generation for problems with deforming geometries, such as ice accreting on aerodynamic surfaces, remains a challenging problem. Here we describe a technique to deform a discrete surface as it evolves due to the accretion of ice. The surface evolution algorithm is based on a smoothed, face-offsetting approach. We also describe a fast algebraic technique to propagate the computed surface deformations into the surrounding volume mesh while maintaining geometric mesh quality. Preliminary results presented here demonstrate the ecacy of the approach for a sphere with a prescribed accretion rate, a rime ice accretion, and a more complex glaze ice accretion.
Document ID
20140005248
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Thompson, David
(Mississippi State Univ. Mississippi State, MS, United States)
Tong, Xiaoling
(Mississippi State Univ. Mississippi State, MS, United States)
Arnoldus, Qiuhan
(Mississippi State Univ. Mississippi State, MS, United States)
Collins, Eric
(Mississippi State Univ. Mississippi State, MS, United States)
McLaurin, David
(Mississippi State Univ. Mississippi State, MS, United States)
Luke, Edward
(Mississippi State Univ. Mississippi State, MS, United States)
Bidwell, Colin S.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
May 8, 2014
Publication Date
June 24, 2013
Subject Category
Aerodynamics
Report/Patent Number
GRC-E-DAA-TN9768
Report Number: GRC-E-DAA-TN9768
Meeting Information
Meeting: Atmospheric and Space Envronments Conference
Location: San Diego, CA
Country: United States
Start Date: June 24, 2013
End Date: June 27, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS-648987.02.03.03.66
CONTRACT_GRANT: NNX12AC22A
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
ice accretion
discrete surface
Icing
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