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Geometry Modeling and Grid Generation for Computational Aerodynamic Simulations Around Iced Airfoils and WingsIssues associated with analysis of 'icing effects' on airfoil and wing performances are discussed, along with accomplishments and efforts to overcome difficulties with ice. Because of infinite variations of ice shapes and their high degree of complexity, computational 'icing effects' studies using available software tools must address many difficulties in geometry acquisition and modeling, grid generation, and flow simulation. The value of each technology component needs to be weighed from the perspective of the entire analysis process, from geometry to flow simulation. Even though CFD codes are yet to be validated for flows over iced airfoils and wings, numerical simulation, when considered together with wind tunnel tests, can provide valuable insights into 'icing effects' and advance our understanding of the relationship between ice characteristics and their effects on performance degradation.
Document ID
20020071136
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Choo, Yung K.
(NASA Glenn Research Center Cleveland, OH United States)
Slater, John W.
(NASA Glenn Research Center Cleveland, OH United States)
Vickerman, Mary B.
(NASA Glenn Research Center Cleveland, OH United States)
VanZante, Judith F.
(QSS Group, Inc. Cleveland, OH United States)
Wadel, Mary F.
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Air Transportation And Safety
Meeting Information
Meeting: 8th International Conference on Numerical Grid Generation in Computational Field Simulations
Location: Honolulu, HI
Country: United States
Start Date: June 3, 2002
End Date: June 6, 2002
Funding Number(s)
PROJECT: RTOP 708-20-13
Distribution Limits
Public
Copyright
Public Use Permitted.
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