|
|
|
|
| LEADER |
03532nam a22005655i 4500 |
| 001 |
7545 |
| 003 |
DE-He213 |
| 005 |
20130725193755.0 |
| 007 |
cr nn 008mamaa |
| 008 |
100301s2009 gw | s |||| 0|eng d |
| 020 |
# |
# |
|a 9783642040931
|9 978-3-642-04093-1
|
| 024 |
7 |
# |
|a 10.1007/978-3-642-04093-1
|2 doi
|
| 050 |
# |
4 |
|a TL787-4050.22
|
| 072 |
# |
7 |
|a TRP
|2 bicssc
|
| 072 |
# |
7 |
|a TTDS
|2 bicssc
|
| 072 |
# |
7 |
|a TEC002000
|2 bisacsh
|
| 082 |
0 |
4 |
|a 629.1
|2 23
|
| 100 |
1 |
# |
|a Kroll, Norbert.
|e editor.
|
| 245 |
1 |
0 |
|a MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design
|b Results of the closing symposium of the MEGADESIGN and MegaOpt projects, Braunschweig, Germany, 23 - 24 May, 2007 /
|c edited by Norbert Kroll, Dieter Schwamborn, Klaus Becker, Herbert Rieger, Frank Thiele.
|h [electronic resource] :
|
| 264 |
# |
1 |
|a Berlin, Heidelberg :
|b Springer Berlin Heidelberg,
|c 2009.
|
| 300 |
# |
# |
|b online resource.
|
| 336 |
# |
# |
|a text
|b txt
|2 rdacontent
|
| 337 |
# |
# |
|a computer
|b c
|2 rdamedia
|
| 338 |
# |
# |
|a online resource
|b cr
|2 rdacarrier
|
| 347 |
# |
# |
|a text file
|b PDF
|2 rda
|
| 490 |
1 |
# |
|a Notes on Numerical Fluid Mechanics and Multidisciplinary Design,
|v 107
|x 1612-2909 ;
|
| 505 |
0 |
# |
|a Part I Reduction of Simulation Time -- Part II Improvement of Simulation Quality Universal Wall Functions for Aerodynamic Flows: Turbulence -- Part III Fluid Structure Coupling -- Part IV Improvement of Shape Optimization Strategies -- Part V Aerodynamic and Multidisciplinary Optimization of 3D-Configurations.
|
| 520 |
# |
# |
|a This volume contains results of the German CFD initiative MEGADESIGN which combines CFD development activities from DLR, universities and aircraft industry. Based on the DLR flow solvers FLOWer and TAU the main objectives of the four-years project is to ensure the prediction accuracy with a guaranteed error bandwidth for certain aircraft configurations at design conditions, to reduce the simulation turn-around time for large-scale applications significantly, to improve the reliability of the flow solvers for full aircraft configurations in the complete flight regime, to extend the flow solvers to allow for multidisciplinary simulations and to establish numerical shape optimization as a vital tool within the aircraft design process. This volume highlights recent improvements and enhancements of the flow solvers as well as new developments with respect to aerodynamic and multidisciplinary shape optimization. Improved numerical simulation capabilities are demonstrated by several industrial applications.
|
| 650 |
# |
0 |
|a Engineering.
|
| 650 |
# |
0 |
|a Engineering mathematics.
|
| 650 |
# |
0 |
|a Hydraulic engineering.
|
| 650 |
# |
0 |
|a Engineering design.
|
| 650 |
# |
0 |
|a Astronautics.
|
| 650 |
1 |
4 |
|a Engineering.
|
| 650 |
2 |
4 |
|a Aerospace Technology and Astronautics.
|
| 650 |
2 |
4 |
|a Engineering Fluid Dynamics.
|
| 650 |
2 |
4 |
|a Appl.Mathematics/Computational Methods of Engineering.
|
| 650 |
2 |
4 |
|a Engineering Design.
|
| 700 |
1 |
# |
|a Schwamborn, Dieter.
|e editor.
|
| 700 |
1 |
# |
|a Becker, Klaus.
|e editor.
|
| 700 |
1 |
# |
|a Rieger, Herbert.
|e editor.
|
| 700 |
1 |
# |
|a Thiele, Frank.
|e editor.
|
| 710 |
2 |
# |
|a SpringerLink (Online service)
|
| 773 |
0 |
# |
|t Springer eBooks
|
| 776 |
0 |
8 |
|i Printed edition:
|z 9783642040924
|
| 830 |
# |
0 |
|a Notes on Numerical Fluid Mechanics and Multidisciplinary Design,
|v 107
|x 1612-2909 ;
|
| 856 |
4 |
0 |
|u https://ezaccess.library.uitm.edu.my/login?url=http://dx.doi.org/10.1007/978-3-642-04093-1
|
| 912 |
# |
# |
|a ZDB-2-ENG
|
| 950 |
# |
# |
|a Engineering (Springer-11647)
|