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Turbomachinery Flow Physics and Dynamic Performance (Record no. 11695)

000 -LEADER
fixed length control field 02834nam a22004095i 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20140310143349.0
007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION
fixed length control field cr nn 008mamaa
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 120430s2012 gw | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number 9783642246753
978-3-642-24675-3
082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 620.1064
Edition number 23
264 #1 -
-- Berlin, Heidelberg :
-- Springer Berlin Heidelberg,
-- 2012.
912 ## -
-- ZDB-2-ENG
100 1# - MAIN ENTRY--PERSONAL NAME
Personal name Schobeiri, Meinhard T.
Relator term author.
245 10 - IMMEDIATE SOURCE OF ACQUISITION NOTE
Title Turbomachinery Flow Physics and Dynamic Performance
Medium [electronic resource] /
Statement of responsibility, etc by Meinhard T. Schobeiri.
250 ## - EDITION STATEMENT
Edition statement 2nd ed. 2012.
300 ## - PHYSICAL DESCRIPTION
Extent XXVI, 725p. 438 illus., 39 illus. in color.
Other physical details online resource.
505 0# - FORMATTED CONTENTS NOTE
Formatted contents note I Turbomachinery Flow Physics -- II Turbomachinery Losses, Efficiencies, Blades -- III Turbomachinery Dynamic Performance -- IV Turbomachinery CFD-Essentials.
520 ## - SUMMARY, ETC.
Summary, etc With 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 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name as entry element Engineering.
Topical term or geographic name as entry element Hydraulic engineering.
Topical term or geographic name as entry element Engineering.
Topical term or geographic name as entry element Engineering Fluid Dynamics.
Topical term or geographic name as entry element Machinery and Machine Elements.
Topical term or geographic name as entry element Fluid- and Aerodynamics.
710 2# - ADDED ENTRY--CORPORATE NAME
Corporate name or jurisdiction name as entry element SpringerLink (Online service)
773 0# - HOST ITEM ENTRY
Title Springer eBooks
776 08 - ADDITIONAL PHYSICAL FORM ENTRY
Display text Printed edition:
International Standard Book Number 9783642246746
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier http://dx.doi.org/10.1007/978-3-642-24675-3
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme
Item type E-Book
Copies
Price effective from Permanent location Date last seen Not for loan Date acquired Source of classification or shelving scheme Koha item type Damaged status Lost status Withdrawn status Current location Full call number
2014-04-02AUM Main Library2014-04-02 2014-04-02 E-Book   AUM Main Library620.1064

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