000 03015nam a22004695i 4500
001 978-3-642-24675-3
003 DE-He213
005 20140220083304.0
007 cr nn 008mamaa
008 120430s2012 gw | s |||| 0|eng d
020 _a9783642246753
_9978-3-642-24675-3
024 7 _a10.1007/978-3-642-24675-3
_2doi
050 4 _aTA357-359
072 7 _aTGMF
_2bicssc
072 7 _aTGMF1
_2bicssc
072 7 _aTEC009070
_2bisacsh
072 7 _aSCI085000
_2bisacsh
082 0 4 _a620.1064
_223
100 1 _aSchobeiri, Meinhard T.
_eauthor.
245 1 0 _aTurbomachinery Flow Physics and Dynamic Performance
_h[electronic resource] /
_cby Meinhard T. Schobeiri.
250 _a2nd ed. 2012.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg,
_c2012.
300 _aXXVI, 725p. 438 illus., 39 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
505 0 _aI Turbomachinery Flow Physics -- II Turbomachinery Losses, Efficiencies, Blades -- III Turbomachinery Dynamic Performance -- IV Turbomachinery CFD-Essentials.
520 _aWith this second revised and extended edition, the readers have a solid source of information for designing state-of-the art turbomachinery components and systems at hand.   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 principles 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.   While maintaining the unifying character of the book structure in this second revised and extended edition all chapters have undergone a rigorous update and enhancement. Accounting for the need of the turbomachinery community, three chapters have been added, that deal with computationally relevant aspects of turbomachinery design such as boundary layer transition, turbulence and boundary layer.
650 0 _aEngineering.
650 0 _aHydraulic engineering.
650 1 4 _aEngineering.
650 2 4 _aEngineering Fluid Dynamics.
650 2 4 _aMachinery and Machine Elements.
650 2 4 _aFluid- and Aerodynamics.
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9783642246746
856 4 0 _uhttp://dx.doi.org/10.1007/978-3-642-24675-3
912 _aZDB-2-ENG
999 _c102321
_d102321