Unsteady Aerodynamic Modeling of A Maneuvering Aircraft Using Indicial Functions

The generation of reduced-order models for the evaluation of unsteady and nonlinear aerodynamic loads is investigated. This approach is based on Duhamels superposition integral using indicial response functions. The indicial functions are directly calculated using the results of unsteady Reynolds-av...

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Bibliographische Detailangaben

Hauptverfasser:	Dan,Rao, Zhenghong,Gao, Senlin,Chen, Fang,Xu, Baigang,Mi
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft computational fluid dynamics Fluid Mechanics indicial response mathematical models nonlinear aerodynamics rom(reduced order model) simulations unsteady aerodynamics
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