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- W3028978808 abstract "After the emergence of a new generation of parallel computers, the capabilities of simultaneous execution of two or more large simulation codes have been increased. Especially in aircraft industries, multidisciplinary optimization technologies are being explored and many advanced researches associated with aero-structural coupled computing can be found. A high-speed aircraft in transonic regime suffers a large increase in wave drag associated with a shock formation. It affects aerodynamic loads and stability-and-control of an aircraft, and is considered serious from the viewpoint of safety and economy. For this situation the simulation should take into account the effects of airframe mass inertia, changes in pressure distribution and wake vortex, or shock formations and movements. These problems are solved by using an unsteady compressible flow solver with moving grid capabilities, a structural solver based on direct-time-integration-method, and grid generator which combines flow field and structure. The system is designed to utilize a parametric configuration of an aircraft, aiming to be used as a preliminary design tool. Loose coupling of computational fluid dynamics (CFD) and computational structural dynamics (CSD) has an advantage in applying the best suited computational methods for each domain. Both domains are computed efficiently on parallel computers by executing fluid and structural equations simultaneously." @default.
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- W3028978808 date "1997-01-01" @default.
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- W3028978808 title "Development of Parallel Computing Environment for Aircraft Aero-Structural Coupled Analysis." @default.
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