Online Projective Integral with Proper Orthogonal Decomposition for Incompressible Flows Past NACA0012 Airfoil
The projective integration method based on the Galerkin-free framework with the assistance of proper orthogonal decomposition (POD) is presented in this paper. The present method is applied to simulate two-dimensional incompressible fluid flows past the NACA0012 airfoil problem. The approach consist...
Saved in:
Main Authors: | Sirod Sirisup, Montri Maleewong |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2012-01-01
|
Series: | Modelling and Simulation in Engineering |
Online Access: | http://dx.doi.org/10.1155/2012/264693 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Improving transonic performance with adjoint-based NACA 0012 airfoil design optimization
by: Efstratios L. Ntantis, et al.
Published: (2024-12-01) -
Aerodynamic Performance of NACA 662-015 Airfoil with Gurney Flap
by: Balram Mandal, et al.
Published: (2024-12-01) -
Experimental Aerodynamics of a NACA 4424 Airfoil at Low Reynolds Number Flow
by: Odenir de Almeida, et al.
Published: (2024-12-01) -
Proper Orthogonal Decomposition as Surrogate Model for Aerodynamic Optimization
by: Valentina Dolci, et al.
Published: (2016-01-01) -
Proper Orthogonal Decomposition Analysis and Dispersion Characteristics of Resonant Acoustic Flow
by: Xiaopeng Wang, et al.
Published: (2020-01-01)