Wing Flutter Tests by a Segmented Aerofoil Model
نویسندگان
چکیده
منابع مشابه
Calculation of Wing Flutter by a Coupled Fluid-Structure Method
An integrated computational uid dynamics (CFD) and computational structural dynamics (CSD) method is developed for the simulation and prediction of utter. The CFD solver is based on an unsteady, parallel, multiblock, multigrid nite volume algorithm for the Euler/Navier–Stokes equations. The CSD solver is based on the time integration of modal dynamic equations extracted from full nite e...
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ژورنال
عنوان ژورنال: The Journal of the Japan Society of Aeronautical Engineering
سال: 1961
ISSN: 1883-5422
DOI: 10.2322/jjsass1953.9.213