LESFOIL: Large Eddy Simulation of Flow Around a High Lift Airfoil: Results of the Project LESFOIL Supported by the European Union 1998 – 2001: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, cartea 83
Editat de Lars Davidson, Davor Cokljat, Jochen Fröhlich, Michael A. Leschziner, Chris Mellen, Wolfgang Rodien Limba Engleză Hardback – 9 mai 2003
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Specificații
ISBN-13: 9783540005339
ISBN-10: 3540005331
Pagini: 264
Ilustrații: XI, 248 p.
Dimensiuni: 155 x 235 x 20 mm
Greutate: 0.54 kg
Ediția:2003
Editura: Springer Berlin, Heidelberg
Colecția Springer
Seria Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Locul publicării:Berlin, Heidelberg, Germany
ISBN-10: 3540005331
Pagini: 264
Ilustrații: XI, 248 p.
Dimensiuni: 155 x 235 x 20 mm
Greutate: 0.54 kg
Ediția:2003
Editura: Springer Berlin, Heidelberg
Colecția Springer
Seria Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Locul publicării:Berlin, Heidelberg, Germany
Public țintă
Professional/practitionerCuprins
I. Introduction.- II. Preparatory Work.- 1 Task 1: Subgrid models.- 2 Task 2: Near-wall models.- 3 Task 4: Numerical methods.- III. The Airfoil Investigations.- 4 Task 5: Airfoil Computations.- IV. Lessons Learned.- 5 Synthesis of the Airfoil Flow Simulations.- V. Conclusions and Outlook.- VI. References.- VII. Addresses of Partners.
Textul de pe ultima copertă
This volume contains results of a European project on Large Eddy Simulation (LES) of the flow around an airfoil. The main objective of the LESFOIL project was to assess the suitability of LES for airfoil flow. In conclusion, preliminary work was carried out such as development of numerical methods, and subgrid modelling in geometrically simple flows such as fully developed channel flow and periodic flow in a channel with a curved hill-shaped surface. Accurate LES of wall-bounded flow requires fine cells in the near-wall region in all coordinate directions. In an attempt to release this constraint, a large part of the LESFOIL project was aimed at developing and validating different approximate near-wall treatments. In the second half of the book, several LESs of the flow around the Aerospatiale-A airfoil are presented, using different numerical methods, grids, SGS models and near-wall treatments.
Caracteristici
Recent results on Large Eddy Simulation applied for aeronautical flows Includes supplementary material: sn.pub/extras