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LESFOIL: Large Eddy Simulation of Flow Around a High Lift Airfoil: Results of th
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Item specifics
- Condition
- Brand New: A new, unread, unused book in perfect condition with no missing or damaged pages. See all condition definitionsopens in a new window or tab
- ISBN-13
- 9783540005339
- Book Title
- LESFOIL: Large Eddy Simulation of Flow Around a High Lift Airfoil
- ISBN
- 9783540005339
- Subject Area
- Technology & Engineering, Science
- Publication Name
- LESFOIL - Large Eddy Simulation of Flow Around a High Lift Airfoil : Results of the Project Lesfoil Supported by the European Union, 1998-2001
- Publisher
- Springer Berlin / Heidelberg
- Item Length
- 9.3 in
- Subject
- Mechanics / Fluids, Mechanical, System Theory, Aeronautics & Astronautics
- Publication Year
- 2003
- Series
- Notes on Numerical Fluid Mechanics and Multidisciplinary Design Ser.
- Type
- Textbook
- Format
- Hardcover
- Language
- English
- Item Weight
- 42.7 Oz
- Item Width
- 6.1 in
- Number of Pages
- Xi, 248 Pages
About this product
Product Identifiers
Publisher
Springer Berlin / Heidelberg
ISBN-10
3540005331
ISBN-13
9783540005339
eBay Product ID (ePID)
2874869
Product Key Features
Number of Pages
Xi, 248 Pages
Language
English
Publication Name
LESFOIL - Large Eddy Simulation of Flow Around a High Lift Airfoil : Results of the Project Lesfoil Supported by the European Union, 1998-2001
Subject
Mechanics / Fluids, Mechanical, System Theory, Aeronautics & Astronautics
Publication Year
2003
Type
Textbook
Subject Area
Technology & Engineering, Science
Series
Notes on Numerical Fluid Mechanics and Multidisciplinary Design Ser.
Format
Hardcover
Dimensions
Item Weight
42.7 Oz
Item Length
9.3 in
Item Width
6.1 in
Additional Product Features
Intended Audience
Scholarly & Professional
LCCN
2003-042594
Series Volume Number
83
Number of Volumes
1 vol.
Illustrated
Yes
Table Of Content
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.
Synopsis
Large Eddy Simulation is a relatively new and still evolving computatio nal strategy for predicting turbulent flows. It is now widely used in research to elucidate fundamental interactions in physics of turbulence, to predict phe nomena which are closely linked to the unsteady features of turbulence and to create data bases against which statistical closure models can be asses sed. However, its applicability to complex industrial flows, to which statisti cal models are applied routinely, has not been established with any degree of confidence. There is, in particular, a question mark against the prospect of LES becoming an economically tenable alternative to Reynolds-averaged N avier-Stokes methods at practically high Reynolds numbers and in complex geometries. Aerospace flows pose particularly challenging problems to LES, because of the high Reynolds numbers involved, the need to resolve accura tely small-scale features in the thin and often transitional boundary layers developing on aerodynamic surfaces. When the flow also contains a separated region - due to high incidence, say - the range and disparity of the influen tial scales to be resolved is enormous, and this substantially aggravates the problems of resolution and cost. It is just this combination of circumstances that has been at the heart of the project LESFOIL to which this book is devoted. The project combined the efforts, resources and expertise of 9 partner organisations, 4 universities, 3 industrial companies and 2 research institu tes., Large Eddy Simulation is a relatively new and still evolving computatio- nal strategy for predicting turbulent flows. It is now widely used in research to elucidate fundamental interactions in physics of turbulence, to predict phe- nomena which are closely linked to the unsteady features of turbulence and to create data bases against which statistical closure models can be asses- sed. However, its applicability to complex industrial flows, to which statisti- cal models are applied routinely, has not been established with any degree of confidence. There is, in particular, a question mark against the prospect of LES becoming an economically tenable alternative to Reynolds-averaged N avier-Stokes methods at practically high Reynolds numbers and in complex geometries. Aerospace flows pose particularly challenging problems to LES, because of the high Reynolds numbers involved, the need to resolve accura- tely small-scale features in the thin and often transitional boundary layers developing on aerodynamic surfaces. When the flow also contains a separated region - due to high incidence, say - the range and disparity of the influen- tial scales to be resolved is enormous, and this substantially aggravates the problems of resolution and cost. It is just this combination of circumstances that has been at the heart of the project LESFOIL to which this book is devoted. The project combined the efforts, resources and expertise of 9 partner organisations, 4 universities, 3 industrial companies and 2 research institu- tes.
LC Classification Number
TA357-359
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