000 03650nam a22003735i 4500
001 299974
003 MX-SnUAN
005 20160429155610.0
007 cr nn 008mamaa
008 150903s2010 gw | o |||| 0|eng d
020 _a9783642040887
_99783642040887
024 7 _a10.1007/9783642040887
_2doi
035 _avtls000353815
039 9 _a201509030508
_bVLOAD
_c201405060326
_dVLOAD
_y201402181002
_zstaff
040 _aMX-SnUAN
_bspa
_cMX-SnUAN
_erda
050 4 _aTA357-359
100 1 _aSchröder, Wolfgang.
_eeditor.
_9337149
245 1 0 _aSummary of Flow Modulation and Fluid-Structure Interaction Findings :
_bResults of the Collaborative Research Center SFB 401 at the RWTH Aachen University, Aachen, Germany, 1997-2008 /
_cedited by Wolfgang Schröder.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg,
_c2010.
300 _a420 páginas 294 ilustraciones
_brecurso en línea.
336 _atexto
_btxt
_2rdacontent
337 _acomputadora
_bc
_2rdamedia
338 _arecurso en línea
_bcr
_2rdacarrier
347 _aarchivo de texto
_bPDF
_2rda
490 0 _aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,
_x1612-2909 ;
_v109
500 _aSpringer eBooks
505 0 _aVortex Sheets of Aircraft in Takeoff and Landing -- An Adaptive Implicit Finite Volume Scheme for Compressible Turbulent Flows about Elastic Configurations -- Timestep Control for Weakly Instationary Flows -- Adaptive Multiscale Methods for Flow Problems: Recent Developments -- Interaction of Wing-Tip Vortices and Jets in the Extended Wake -- Experimental and Numerical Investigation of Unsteady Transonic Airfoil Flow -- Enabling Technologies for Robust High-Performance Simulations in Computational Fluid Dynamics -- Influencing Aircraft Wing Vortices -- Development of a Modular Method for Computational Aero-structural Analysis of Aircraft -- A Unified Approach to the Modeling of Airplane Wings and Numerical Grid Generation Using B-Spline Representations -- Parallel and Adaptive Methods for Fluid-Structure-Interactions -- Iterative Solvers for Discretized Stationary Euler Equations -- Unsteady Transonic Fluid - Structure - Interaction at the BAC 3-11 High Aspect Ratio Swept Wing -- Structural Idealization of Flexible Generic Wings in Computational Aeroelasticity -- Aero-structural Dynamics Experiments at High Reynolds Numbers.
520 _aThe Collaborative Research Center SFB 401: Flow Modulation and Fluid-Structure Interaction at Airplane Wings investigates numerically and experimentally fundamental problems of very high capacity aircraft having large elastic wings. This issue summarizes the findings of the 12-year research program at RWTH Aachen University which was funded by the Deutsche Forschungsgemeinschaft (DFG) from 1997 through 2008. The research program covered the following three main topics of large transport aircraft: (i) Model flow, wakes, and vortices of airplanes in high-lift-configuration, (ii) Numerical tools for large scale adaptive flow simulation based on multiscale analysis and a parametric mapping concept for grid generation, and (iii) Validated computational design tools based on direct aeroelastic simulation with reduced structural models.
590 _aPara consulta fuera de la UANL se requiere clave de acceso remoto.
710 2 _aSpringerLink (Servicio en línea)
_9299170
776 0 8 _iEdición impresa:
_z9783642040870
856 4 0 _uhttp://remoto.dgb.uanl.mx/login?url=http://dx.doi.org/10.1007/978-3-642-04088-7
_zConectar a Springer E-Books (Para consulta externa se requiere previa autentificación en Biblioteca Digital UANL)
942 _c14
999 _c299974
_d299974