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000751631 019__ $$a931578205$$a932321713
000751631 020__ $$a9783319211275$$q(electronic book)
000751631 020__ $$a3319211277$$q(electronic book)
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000751631 08204 $$a629.134/32$$223
000751631 24500 $$aAdvances in simulation of wing and nacelle stall$$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.
000751631 264_1 $$a[Cham] :$$bSpringer,$$c[2015]
000751631 264_4 $$c©2016
000751631 300__ $$a1 online resource (ix, 413 pages) :$$billustrations.
000751631 336__ $$atext$$btxt$$2rdacontent
000751631 337__ $$acomputer$$bc$$2rdamedia
000751631 338__ $$aonline resource$$bcr$$2rdacarrier
000751631 4901_ $$aNotes on numerical fluid mechanics and multidisciplinary design,$$x1612-2909 ;$$vvolume 131
000751631 504__ $$aIncludes bibliographical references and author index.
000751631 5050_ $$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.
000751631 506__ $$aAccess limited to authorized users.
000751631 520__ $$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.
000751631 588__ $$aOnline resource; title from title details screen (SpringerLink, viewed July 17, 2015).
000751631 650_0 $$aAirplanes$$xWings$$vCongresses.
000751631 650_0 $$aAirplanes$$xNacelles$$vCongresses.
000751631 7001_ $$aRadespiel, Rolf,$$eeditor.
000751631 7001_ $$aNiehuis, Reinhard,$$eeditor.
000751631 7001_ $$aKroll, Norbert,$$eeditor.
000751631 7001_ $$aBehrends, Kathrin,$$eeditor.
000751631 77608 $$iPrint version:$$tAdvances in simulation of wing and nacelle stall : results of the closing symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany.$$dCham, Switzerland : Springer, c2016$$z9783319211268
000751631 830_0 $$aNotes on numerical fluid mechanics and multidisciplinary design ;$$vvolume 131.
000751631 852__ $$bebk
000751631 85640 $$3SpringerLink$$uhttps://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-3-319-21127-5$$zOnline Access$$91397441.1
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