Summary
The numerical analysis of aerodynamic flows is in general limited to steady geometries. Depending on the flow conditions steady or transient flow solutions in the relative frame of the body are computed. In order to take into account the flexibility of the body (e.g. fluttering wing) and the motion of the body (manoeuvre flight), moving computational meshes are required. The CFD method has to take into account meshes with moving nodes and deforming control volumes. The present paper shows computational results of different applications with moving grids, e.g. an oscillating airfoil, a fluttering wing and a guided manoeuvre flight of an airplane.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
Similar content being viewed by others
References
T.J. Barth and D.C. Jesperson. The design and application of upwind schemes on unstructured meshes. AIAA Paper 89-0366, 1989.
Breitsamter. Vortical Flow Field Structures at Forward Swept Wing Configurations. ICAS Proceedings 1998, 21st Congress, Melbourne, Australia, 1998
CFX-5.7 Solver Manual. ANSYS Inc., 2004.
I. Demirdzic and M. Peric. Space con~rvation law in finite volume calculations of fluid flow. Int. J. Num. Methods in Fluids, 8, pp1037–1050, 1998.
C. Gao, S. Luo, E Liu and D.M. Schuster. Calculation of Unsteady Transonic Flow by and Euler Method with Small Perturbation Boundary Conditions. AIAA 03-1267, 2003.
H. Grotjans and ER. Menter. Wall Functions for General Application CFD Codes. Computational Fluid Dynamics, Proceedings of the 4th Computational Fluid Dynamics conference, 7-11 Sept. 1998, Athens, Greece, Vol. 1, Part 2, ECCOMAS, John Wiley & Sons, pp. 1112–1, 1998.
W. Haase, V. Selmin, B. Winzell. Progress in Computational Flow-Structure Interaction. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Springer, Volume 81, 2003
LR. Hawkings and N.S. Wilkes. Moving Grids in HarwelI-FLOW3D. AEA, InTec-0608, 1991.
R.H. Landon. NACA0012 Oscillatory and Transient Pitching, Compendium of Unsteady Aerodynamic Measurements, Data Set 3. AGARD Report R-702, Aug. 1982.
R. Langtry, Drag Prediction of Engine-Airframe Interference Effects with CFX-5, AIAA 2004-0391.
M.J. Raw. Robustness of coupled algebraic muitigrid for the Navier-Stokes equations. AIAA Paper 96-0297, 1996.
C,M. Rhie and W.L. Chow. Numerical study of the turtmlent flow past an airfoil with trailing edge separation. AIAA Journal, 21:1525-1532, 1983.
G.E. Schneider and M.J. Raw. Control volume finite-element method for heat transfer and fluid flow using colocated variables. 1. Computational procedure. Numerical Heat Transfer, 11:363–390, 1987.
E.C. Yates. AGARD Standard Aeroelastic Configuration for Dynamic Response, I, Wing 445.6. AGARD-R-765, 1988.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2006 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Kuntz, M., Menter, F.R. (2006). Numerical Flow Simulation with Moving Grids. In: Rath, HJ., Holze, C., Heinemann, HJ., Henke, R., Hönlinger, H. (eds) New Results in Numerical and Experimental Fluid Mechanics V. Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), vol 92. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-33287-9_54
Download citation
DOI: https://doi.org/10.1007/978-3-540-33287-9_54
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-33286-2
Online ISBN: 978-3-540-33287-9
eBook Packages: EngineeringEngineering (R0)