LEADER 05826nam 22007335 450 001 9910254190203321 005 20251230061604.0 010 $a3-319-21127-7 024 7 $a10.1007/978-3-319-21127-5 035 $a(CKB)3710000000444462 035 $a(EBL)3567645 035 $a(SSID)ssj0001534589 035 $a(PQKBManifestationID)11823032 035 $a(PQKBTitleCode)TC0001534589 035 $a(PQKBWorkID)11496480 035 $a(PQKB)10980288 035 $a(DE-He213)978-3-319-21127-5 035 $a(MiAaPQ)EBC3567645 035 $a(PPN)187689989 035 $a(MiAaPQ)EBC6231839 035 $a(EXLCZ)993710000000444462 100 $a20150709d2016 u| 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aAdvances in Simulation of Wing and Nacelle Stall $eResults of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany /$fedited by Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends 205 $a1st ed. 2016. 210 1$aCham :$cSpringer International Publishing :$cImprint: Springer,$d2016. 215 $a1 online resource (404 p.) 225 1 $aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,$x1860-0824 ;$v131 300 $aDescription based upon print version of record. 311 08$a3-319-21126-9 320 $aIncludes bibliographical references at the end of each chapters and index. 327 $aThe Delay of RANS-to-LES Transition in Hybrid RANS-LES Approaches and Some Recently Proposed Remedies -- Computations of Separated Flows with a Hybrid RANS/LES Approach -- Hybrid RANS/LES Study of the Development of an Airfoil-Generated Vortex -- Interaction of Three-Dimensional Disturbances with the Flow around a Two-Element High-Lift Airfoil -- The Discontinuous Galerkin Method as an Enabling Technology for DNS and LES of Industrial Aeronautical Applications -- Body Force Modelling of Internal Geometry for Jet Noise Prediction -- Numerical Studies of Turbulent Flow Influence on a Two-Element Airfoil -- CFD for Prediction of Flow Separation from Aircraft Tail Surfaces -- Zonal RANS-LES Computation for Near-Stall-Airfoil Flow -- Criteria for Crosswind Variations during Approach and Touchdown at Airports -- Development and Improvement of Two Methods of Different Complexity to Simulate Atmospheric Boundary Layer Turbulence for Aircraft Design Studies -- Simulation of Interaction of Aircraft with Gust and Resolved LES-Simulated Atmospheric Turbulence -- A New Method to Generate Anisotropic Synthetic Turbulence for LES -- Numerical Simulation of the Turbulent Flow Around a Wing -- Integration- and Intake-Induced Flow Distortions and their Impact on Aerodynamic Fan Performance -- Flow Investigations in a Stalling Nacelle Inlet Under Disturbed Inflow -- Realistic Inlet Distortion Patterns Interacting with a Transonic Compressor Stage -- Unsteady CFD Simulation of Transonic Axial Compressor Stages with Distorted Inflow -- Transitional Shock-Wave/Boundary-Layer Interactions in Intakes at Incidence.-Advanced Design Approach for a High-lift Wind Tunnel Model Based on Flight Test Data -- Simulation of Longitudinal Vortices on a High-LiftWing -- Impact of Different UHBR-Engine Positions on the Aerodynamics of a High-LiftWing -- Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration -- Numerical Studies of Active Flow Control Applied at the Engine-Wing Junction. 330 $aThe book reports on advanced solutions to the problem of simulating wing and nacelle stall, as presented and discussed by internationally recognized researchers at the Closing Symposium of the DFG Research Unit FOR 1066. Reliable simulations of flow separation on airfoils, wings and powered engine nacelles at high Reynolds numbers represent great challenges in defining suitable mathematical models, computing numerically accurate solutions and providing comprehensive experimental data for the validation of numerical simulations. Additional problems arise from the need to consider airframe-engine interactions and inhomogeneous onset flow conditions, as real aircraft operate in atmospheric environments with often-large distortions. The findings of fundamental and applied research into these and other related issues are reported in detail in this book, which targets all readers, academics and professionals alike, interested in the development of advanced computational fluid dynamics modeling for the simulation of complex aircraft flows with flow separation. 410 0$aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,$x1860-0824 ;$v131 606 $aFluid mechanics 606 $aContinuum mechanics 606 $aAerospace engineering 606 $aAstronautics 606 $aEngineering Fluid Dynamics 606 $aContinuum Mechanics 606 $aAerospace Technology and Astronautics 615 0$aFluid mechanics. 615 0$aContinuum mechanics. 615 0$aAerospace engineering. 615 0$aAstronautics. 615 14$aEngineering Fluid Dynamics. 615 24$aContinuum Mechanics. 615 24$aAerospace Technology and Astronautics. 676 $a629.13432 702 $aRadespiel$b Rolf$4edt$4http://id.loc.gov/vocabulary/relators/edt 702 $aNiehuis$b Reinhard$4edt$4http://id.loc.gov/vocabulary/relators/edt 702 $aKroll$b Norbert$4edt$4http://id.loc.gov/vocabulary/relators/edt 702 $aBehrends$b Kathrin$4edt$4http://id.loc.gov/vocabulary/relators/edt 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910254190203321 996 $aAdvances in Simulation of Wing and Nacelle Stall$91540925 997 $aUNINA