The main objectives of the research was to further develop the necessary fundamental algorithms to enable high fidelity multi-disciplinary design of complete aircraft configurations. The work was focused on four main areas: (1) Flow solution algorithms for unstructured meshes, (2) Aero-structural plan-form optimization, (3) Multi-fidelity approach to multi-disciplinary design of supersonic aircraft. (4) Algorithms for automatic feedback control of aerodynamic flows.
High-Fidelity Multidisciplinary Design Using an Integrated Design Environment
2007
39 pages
Report
Keine Angabe
Englisch
Aircraft , Aerodynamics , Algebra, Analysis, Geometry, & Mathematical Logic , Algorithms , Configurations , Supersonic aircraft , Control , Optimization , Supersonic flow , Aerodynamic forces , Computations , Feedback , Multidisciplinary design , Computational algorithms , Control of aerodynamic flows
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