000 03231nam a22003615i 4500
001 293777
003 MX-SnUAN
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007 cr nn 008mamaa
008 150903s2005 gw | o |||| 0|eng d
020 _a9783540265917
_99783540265917
024 7 _a10.1007/b137854
_2doi
035 _avtls000346658
039 9 _a201509031116
_bVLOAD
_c201405070508
_dVLOAD
_y201402070902
_zstaff
040 _aMX-SnUAN
_bspa
_cMX-SnUAN
_erda
050 4 _aTA357-359
100 1 _aSchobeiri, Meinhard.
_eautor
_9326717
245 1 0 _aTurbomachinery Flow Physics and Dynamic Performance /
_cby Meinhard Schobeiri.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg :
_bImprint: Springer,
_c2005.
300 _axxI, 522 páginas
_brecurso en línea.
336 _atexto
_btxt
_2rdacontent
337 _acomputadora
_bc
_2rdamedia
338 _arecurso en línea
_bcr
_2rdacarrier
347 _aarchivo de texto
_bPDF
_2rda
500 _aSpringer eBooks
505 0 _aTurbomachinery Flow Physics -- Introduction, Turbomachinery, Applications, Types -- Kinematics of Turbomachinery Fluid Motion -- Differential Balances in Turbomachinery -- Integral Balances in Turbomachinery -- Theory of Turbomachinery Stages -- Turbine and Compressor Cascade Flow Forces -- Turbomachinery Losses, Efficiencies, Blades -- Losses in Turbine and Compressor Cascades -- Efficiency of Multi-stage Turbomachines -- Incidence and Deviation -- Simple Blade Design -- Radial Equilibrium -- Turbomachinery Dynamic Performance -- Nonlinear Dynamic Simulation of Turbomachinery Components and Systems -- Generic Modeling of Turbomachinery Components and Systems -- Modeling of Inlet, Exhaust, and Pipe Systems -- Modeling of Heat Exchangers, Combustion Chambers, Afterburners -- Modeling the Compressor Component, Design and Off-Design -- Turbine Aerodynamic Design and Off-design Performance -- Gas Turbine Engines, Design and Dynamic Performance.
520 _aOver the past three decades turbomachines experienced a steep increase in efficiency and performance. Based on fundamental principles of turbomachinery thermo-fluid mechanics, numerous CFD based calculation methods are being developed to simulate the complex 3-dimensional, highly unsteady turbulent flow within turbine or compressor stages. The objective of this book is to present the fundamental principals of turbomachinery fluid-thermodynamic design process of turbine and compressor components, power generation and aircraft gas turbines in a unified and compact manner. The book provides senior undergraduate students, graduate students and engineers in the turbomachinery industry with a solid background of turbomachinery flow physics and performance fundamentals that are essential for understanding turbomachinery performance and flow complexes.
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:
_z9783540223689
856 4 0 _uhttp://remoto.dgb.uanl.mx/login?url=http://dx.doi.org/10.1007/b137854
_zConectar a Springer E-Books (Para consulta externa se requiere previa autentificación en Biblioteca Digital UANL)
942 _c14
999 _c293777
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