Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1719376 | Progress in Aerospace Sciences | 2011 | 8 Pages |
Abstract
The CEASIOM software developed in the EU-funded collaborative research project SimSAC generates stability and control data for preliminary aircraft design using different methods of varying fidelity. In order to obtain the aerodynamic derivatives by CFD, the aircraft geometry must be defined, computational meshes generated, and numerical parameters set for the flow solvers. An approach to automation of the process is discussed, involving geometry generation and mesh generation for inviscid as well as RANS flow models.
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Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Maximilian Tomac, David Eller,