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- W2368225858 abstract "CFD method has been an important method for aerodynamic analysis.The paper used CFD method to do numerical simulations of Naca0012 airfoil model,and got its aerodynamic coefficients and flutter derivatives.The paper gave out a new effective mesh control method,used self-owned codes and ANSYS-CFX solver to handle fluid-structure interaction.After proving the method was effective through comparisons between theory and CFD,the paper progressed numerical simulations for flutter derivatives identifications using many different force vibration amplitudes.Through these results,the paper discussed the applicable range of Theodorsen theory and the changing trends of flutter derivatives." @default.
- W2368225858 created "2016-06-24" @default.
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- W2368225858 date "2010-01-01" @default.
- W2368225858 modified "2023-09-23" @default.
- W2368225858 title "Aerodynamic Analysis of Naca0012 Airfoil Model using CFD" @default.
- W2368225858 hasPublicationYear "2010" @default.
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