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• W2324699453 abstract "A methodology that enables the investigation of static and dynamic nonlinear aeroelastic phenomena of flight vehicles is presented. A time accurate Euler/Navier Stokes solver is coupled with a general linear structural solver in physical coordinates to solve the equations of motion. For static aeroelastic analysis, a pseudo time approach is employed along with relaxation of the structural deformations to obtain converged solutions. Transient analyses are solved by time marching the fluid and structural equations in a staggered fashion. The methodology is exercised by performing static aeroelastic calculations for two configurations, a generic fighter wing and the Validation of Aeroelastic Tailoring (VAT) wind tunnel model." @default.
• W2324699453 created "2016-06-24" @default.
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• W2324699453 date "2000-09-06" @default.
• W2324699453 modified "2023-09-27" @default.
• W2324699453 title "A methodology of large scale computational aeroelasticity for the MDA/MDO environment" @default.
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• W2324699453 doi "https://doi.org/10.2514/6.2000-4789" @default.
• W2324699453 hasPublicationYear "2000" @default.
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