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Unstructured Grid Generation for Complex 3D High-Lift Configurations

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Pirzadeh, Shahyar Z., author.
Conference Name:
World Aviation Congress & Exposition (1999-10-19 : San Francisco, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1999
Summary:
The application of an unstructured grid methodology on a three-dimensional high-lift configuration is presented. The focus of this paper is on the grid generation aspect of an integrated effort for the development of an unstructured- grid computational fluid dynamics (CFD) capability at the NASA Langley Research Center. The meshing approach is based on tetrahedral grids generated by the advancing-front and the advancing-layers procedures. The capability of the method for solving high-lift problems is demonstrated on an aircraft model referred to as the energy efficient transport configuration. The grid generation issues, including the pros and cons of the present approach, are discussed in relation to the high-lift problems. Limited viscous flow results are presented to demonstrate the viability of the generated grids. A corresponding Navier-Stokes solution capability, along with further computations on the present grid, is presented in a companion SAE paper
Notes:
Vendor supplied data
Publisher Number:
1999-01-5557
Access Restriction:
Restricted for use by site license

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