000 05634nam a22005895i 4500
001 978-3-319-21127-5
003 DE-He213
005 20220801221200.0
007 cr nn 008mamaa
008 150709s2016 sz | s |||| 0|eng d
020 _a9783319211275
_9978-3-319-21127-5
024 7 _a10.1007/978-3-319-21127-5
_2doi
050 4 _aTA357-359
072 7 _aTGMF
_2bicssc
072 7 _aTEC009070
_2bisacsh
072 7 _aTGMF
_2thema
082 0 4 _a620.1064
_223
245 1 0 _aAdvances in Simulation of Wing and Nacelle Stall
_h[electronic resource] :
_bResults of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany /
_cedited by Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends.
250 _a1st ed. 2016.
264 1 _aCham :
_bSpringer International Publishing :
_bImprint: Springer,
_c2016.
300 _aIX, 413 p. 273 illus., 107 illus. in color.
_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,
_x1860-0824 ;
_v131
505 0 _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.
520 _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.
650 0 _aFluid mechanics.
_92810
650 0 _aContinuum mechanics.
_93467
650 0 _aAerospace engineering.
_96033
650 0 _aAstronautics.
_954564
650 1 4 _aEngineering Fluid Dynamics.
_954565
650 2 4 _aContinuum Mechanics.
_93467
650 2 4 _aAerospace Technology and Astronautics.
_954566
700 1 _aRadespiel, Rolf.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_954567
700 1 _aNiehuis, Reinhard.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_954568
700 1 _aKroll, Norbert.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_954569
700 1 _aBehrends, Kathrin.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_954570
710 2 _aSpringerLink (Online service)
_954571
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9783319211282
776 0 8 _iPrinted edition:
_z9783319211268
776 0 8 _iPrinted edition:
_z9783319370675
830 0 _aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,
_x1860-0824 ;
_v131
_954572
856 4 0 _uhttps://doi.org/10.1007/978-3-319-21127-5
912 _aZDB-2-ENG
912 _aZDB-2-SXE
942 _cEBK
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