High Fidelity Multidisciplinary Design Using An Integrated Design Environment
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High-fidelity Multidisciplinary Design Using an Integrated Design Environment
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.
The National Academy of Sciences' Decadal Plan for Aeronautics
Author: United States. Congress. House. Committee on Science. Subcommittee on Space and Aeronautics
language: en
Publisher:
Release Date: 2007
Advances in Structural and Multidisciplinary Optimization
The volume includes papers from the WSCMO conference in Braunschweig 2017 presenting research of all aspects of the optimal design of structures as well as multidisciplinary design optimization where the involved disciplines deal with the analysis of solids, fluids or other field problems. Also presented are practical applications of optimization methods and the corresponding software development in all branches of technology.