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Multi-fidelity modeling framework for nonlinear unsteady aerodynamics of airfoils

  • Published:2019-12 Issue: Volume:76 Page:832-855
  • ISSN:0307-904X
  • Container-title:Applied Mathematical Modelling
  • language:en
  • Short-container-title:Applied Mathematical Modelling

Author:

Kou JiaqingORCID,Zhang WeiweiORCID

Funder

National Natural Science Foundation of China

National Science Fund for Excellent Young Scholars

111 project of China

ATCFD project

Publisher

Elsevier BV

Subject

Applied Mathematics,Modelling and Simulation

Reference82 articles.

1. Ber die entstehung des dynamischen auftriebes von tragflügeln;Wagner;Z. Angew. Math. Mech.,1925

2. T. Theodorsen. General Theory of Aerodynamic Instability and the Mechanism of Flutter. Technical Report, 1935.

3. A doublet lattice method for calculating lift distributions on oscillating surfaces in subsonic flow;Albano;AIAA J.,1969

4. Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics;Murua;Prog. Aerosp. Sci.,2012

5. Analytical methods for the development of reynolds-stress closures in turbulence;Speziale;Annu. Rev. Fluid Mech.,1991

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