000 04348nam a22005655i 4500
001 978-3-540-32382-2
003 DE-He213
005 20160614135155.0
007 cr nn 008mamaa
008 100301s2005 gw | s |||| 0|eng d
020 _a9783540323822
_9978-3-540-32382-2
024 7 _a10.1007/3-540-32382-1
_2doi
049 _aAlfaisal Main Library
050 4 _aTL1-483
072 7 _aTRC
_2bicssc
072 7 _aTRCS
_2bicssc
072 7 _aTEC009090
_2bisacsh
082 0 4 _a629.2
_223
245 1 0 _aMEGAFLOW - Numerical Flow Simulation for Aircraft Design
_h[electronic resource] :
_bResults of the second phase of the German CFD initiative MEGAFLOW, presented during its closing symposium at DLR, Braunschweig, Germany, December 10 and 11, 2002 /
_cedited by Norbert Kroll, Jens K. Fassbender.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg,
_c2005.
300 _aIX, 318 p.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aNotes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM),
_x1612-2909 ;
_v89
505 0 _aGrid Generation -- Hybrid unstructured Grid Generation in MEGAFLOW -- Structured Solver FLOWer -- Block Structured Navier-Stokes Solver FLOWer -- Transition Modeling in FLOWer — Transition Prescription and Prediction -- Turbulence Models in FLOWer -- Hybrid Solver TAU -- Overview of the Hybrid RANS Code TAU -- Algorithmic Developments in TAU -- Hybrid Grid Adaptation in TAU -- Turbulence Model Implementation in TAU -- G.I.G. — A Flexible User-Interface for CFD-Code Configuration Data -- Validation -- Computation of Aerodynamic Coefficients for Transport Aircraft with MEGAFLOW -- Computation of Engine-Airframe Installation Drag -- Verification of MEGAFLOW-Software for High Lift Applications -- Shape Optimization -- The Continuous Adjoint Approach in Aerodynamic Shape Optimization -- Application of the Adjoint Technique with the Optimization Framework Synaps Pointer Pro -- Shape Parametrization Using Freeform Deformation -- Contributions of Universities -- Advanced Turbulence Modelling in Aerodynamic Flow Solvers -- Large-Eddy Simulation of Attached Airfoil Flow -- Transition Prediction for 2D and 3D Flows using the TAU-Code and N-Factor Methods -- Exploitation of MEGAFLOW Software -- Application of the MEGAFLOW Software at DLR -- MEGAFLOW for AIRBUS-D — Applications and Requirements -- Aerodynamic Analysis of Flapping Airfoil Propulsion at Low Reynolds Numbers.
520 _aThis volume contains results of the German CFD initiative MEGAFLOW which combines many of the CFD development activities from DLR, universities and aircraft industry. It highlights recent improvements and enhancements of the MEGAFLOW software system. This software includes the block-structured Navier-Stokes code FLOWer and the unstructured Navier-Stokes code TAU. Improvements to numerical algorithms and physical modelling capabilities of these codes are discussed. Validation activities concerning their capability to predict viscous flows around complex industrially relevant configurations for transport aircraft design are presented. The high level of maturity both codes have reached is demonstrated based on the intensive use of FLOWer and TAU by the German aerospace industry in the design process of a new aircraft.
650 0 _aEngineering.
650 0 _aFluids.
650 0 _aComputational intelligence.
650 0 _aFluid mechanics.
650 0 _aAutomotive engineering.
650 1 4 _aEngineering.
650 2 4 _aAutomotive Engineering.
650 2 4 _aComputational Intelligence.
650 2 4 _aEngineering Fluid Dynamics.
650 2 4 _aFluid- and Aerodynamics.
655 7 _aElectronic books.
_2local
700 1 _aKroll, Norbert.
_eeditor.
700 1 _aFassbender, Jens K.
_eeditor.
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9783540243830
830 0 _aNotes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM),
_x1612-2909 ;
_v89
856 4 0 _uhttp://ezproxy.alfaisal.edu/login?url=http://dx.doi.org/10.1007/3-540-32382-1
912 _aZDB-2-ENG
942 _2lcc
_cEBOOKS
999 _c245683
_d245683