Home DE ES FR


Advanced Search

Our On-Line PhDs

Submit a Thesis
My Account Register Help

About
Fields
Mathematics and Applications
Information and Communication Sciences and Technologies
Physics, Optics
Materials Science, Mechanics and Mechanical Engineering
Fluid Mechanics and Energy
Chemistry, Physical Chemistry and Chemical Engineering
Life Sciences and Engineering
Earth Sciences and Environmental Engineering
Sciences of Economy, Management and Society
Vorticity preserving numerical schemes in compressible aerodynamics

Falissard, Fabrice (2006) Vorticity preserving numerical schemes in compressible aerodynamics. PhD thesis Mécanique, ENSAM 2006ENAM0005.

Full text available as:

- These_Falissard.pdf ( 9720 Kb )
Licence: Copyright

Abstract

The reduction of numerical diffusion of vortex structures is a key point in many computational fluid dynamics problems. According to the notion of vorticity preserving numerical schemes for the system wave equation, introduced by Morton and Roe, and on the residual-based schemes family, introduced by Lerat and Corre, this thesis presents a RBV scheme (Residual- Based Vorticity preserving). The RBV scheme is implicit and second order accurate. It preserves the vorticity for the system wave equation with and without advection and for the Euler equations. The RBV scheme has the capability of advecting vortex on large distances with very few numerical dissipation. It has been formulated on irregular grids in the finite volume approach and it retains naturally its accuracy and vorticity preserving properties without correction terms. The RBV scheme has been used first for the calculation of steady and unsteady Euler flow around airfoils and then for the simulation of subsonic head-on blade vortex interaction (BVI) between a Scully vortex and a NACA0012 airfoil at zero angle of attack. Results are compared to experimental data. This case is representative of the parallel interaction between a helicopter rotor blade and the preceding blade tip vortex. The blade vortex interaction is the main noise source for helicopter in low speed descent flight. The results obtained with the RBV scheme on this two-dimensional BVI case show the capability of the method to simulate realistic aerodynamic flows. Comparisons made with solutions of classical second order accurate schemes demonstrate the benefit of the proposed RBV scheme.

Item Type:PhD Thesis (PhD)
Thesis Supervisor:Lerat, Alain
Date:January 2006
Board of examiners:Abgrall, Rémi and Darracq, Denis and Huberson, Serge and Lerat, Alain and Piquet, Jean and Sidès, Jacques
Ecole Doctorale:ED 432 ECOLE DOCTORALE SCIENCES DES METIERS DE L'INGENIEUR
Discipline:Mécanique
Collection (Fonds):ENSAM
Institution:ENSAM
Subjects:4. Materials Science, Mechanics and Mechanical Engineering
Uncontrolled Keywords:Residual-based scheme, Finite-volume method, Vortex capturing, Aerodynamics, Compressible flow, Steady flow, Unsteady flow, Bvi, Schéma basé sur le résidu, Volumes finis, Tourbillon, Vorticité, Aérodynamique, écoulement compressible, écoulement stationnaire, écoulement instationnaire, Interaction paletourbillon
ID Code:2056
Deposited By:Christine Ollendorff
Deposited On:05 January 2007

Statistiques de consultation

Repository Staff Only: edit this item

© ParisTech 2007 - Réalisé par RILK.com - Graphisme par Winch Communication