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  • 1
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    Unknown
    In:  CASI
    Publication Date: 2019-07-27
    Description: The purpose of this paper is to present an algorithm for using NonUniform Rational B-Spline (NURBS) representation in an aeroelastic loop. The algorithm is based on creating a least-squares NURBS surface representing the aeroelastic defection. The resulting NURBS surfaces are used to update either the original Computer- Aided Design (CAD) model, Computational Structural Mechanics (CSM) grid or the Computational Fluid Dynamics (CFD) grid. Results are presented for a generic High-Speed Civil Transport (HSCT).
    Keywords: Aerodynamics
    Type: 6th International Conference on Numerical Grid Generation in Computational Field Simulation; 6-9 Jul. Jul. 1998; London; United Kingdom
    Format: application/pdf
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