作者: Earl H. Dowell , Kenneth C. Hall , Jeffrey P. Thomas , Robert E. Kielb , Meredith A. Spiker
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摘要: The state of reduced order modeling unsteady aerodynamic flows for the efficient calculation fluid-structure interaction (aeroelasticity) is discussed. Reduced a set conceptually novel and computationally techniques computing flow about airfoils, wings, turbomachinery cascades.