DocumentCode :
1593610
Title :
Investigation of NND Scheme for Transonic CFDCSD Interaction Problems
Author :
Hasham, Hasan Junaid ; Khawar, Jawad ; Bai, Zhang Jin ; Ming, Xu Yuan
Author_Institution :
Dept. of Aeronaut., Beihang Univ., Beijing, China
Volume :
3
fYear :
2010
Firstpage :
19
Lastpage :
23
Abstract :
The aim of the paper is to validate the implicit finite difference NND scheme, first developed in early 1990´s for use in CFD-CSD interaction problems. The focus was on implementing the existing numerical scheme of NND for validating the unsteady flow over NACA0012 airfoil using thin-layer Navier-Stokes equation. The equation was coupled with the structural dynamic model to identify the conventional flutter boundary and the behavior of the scheme near the flutter points. The results show that all the features of the unsteady flow have been captured.
Keywords :
Navier-Stokes equations; aerodynamics; computational fluid dynamics; elasticity; finite difference methods; flow instability; transonic flow; NACA0012 airfoil; aeroelasticity; flutter boundary; implicit finite difference NND scheme; structural dynamic model; thin-layer Navier-Stokes equation; transonic CFD-CSD interaction problems; unsteady flow; Aerodynamics; Automotive components; Computational fluid dynamics; Computational modeling; Computer simulation; Differential equations; Navier-Stokes equations; Neutron spin echo; Projectiles; Vehicles; CFDCSD; LUSGS; NND Scheme; Runge-Kutta IV Method;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Modeling and Simulation, 2010. ICCMS '10. Second International Conference on
Conference_Location :
Sanya, Hainan
Print_ISBN :
978-1-4244-5642-0
Electronic_ISBN :
978-1-4244-5643-7
Type :
conf
DOI :
10.1109/ICCMS.2010.380
Filename :
5421170
Link To Document :
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