Reduced-Order Nonlinear Unsteady Aerodynamic Modeling Using a Surrogate-Based Recurrence Framework

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Reduced-Order Nonlinear Unsteady Aerodynamic Modeling Using a Surrogate-Based Recurrence Framework

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ژورنال

عنوان ژورنال: AIAA Journal

سال: 2010

ISSN: 0001-1452,1533-385X

DOI: 10.2514/1.j050471