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Principles of turbomachinery / (Record no. 29749)

000 -LEADER
fixed length control field 04352cam a2200301Mu 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20190228114013.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 120109s2011 nju ob 001 0 eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number 9780470536728
041 ## - Language
Language code of text/sound track or separate title eng
050 #4 - LIBRARY OF CONGRESS CALL NUMBER
Classification number TJ267
Classification number TJ267
082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 621.406
Item number K849
100 1# - MAIN ENTRY--PERSONAL NAME
Personal name Korpela, Seppo A.
9 (RLIN) 28325
245 10 - IMMEDIATE SOURCE OF ACQUISITION NOTE
Title Principles of turbomachinery /
Statement of responsibility, etc Seppo A. Korpela.
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Place of publication, distribution, etc Hoboken, N.J :
Name of publisher, distributor, etc Wiley,
Date of publication, distribution, etc 2011.
300 ## - PHYSICAL DESCRIPTION
Extent xvi, 457 p. ;
Dimensions 24 cm.
504 ## - BIBLIOGRAPHY, ETC. NOTE
Bibliography, etc Includes bibliographical references and index.
505 0# - FORMATTED CONTENTS NOTE
Formatted contents note Principles of Turbomachinery; CONTENTS; Foreword; Acknowledgments; 1 Introduction; 1.1 Energy and fluid machines; 1.1.1 Energy conversion of fossil fuels; 1.1.2 Steam turbines; 1.1.3 Gas turbines; 1.1.4 Hydraulic turbines; 1.1.5 Wind turbines; 1.1.6 Compressors; 1.1.7 Pumps and blowers; 1.1.8 Other uses and issues; 1.2 Historical survey; 1.2.1 Water power; 1.2.2 Wind turbines; 1.2.3 Steam turbines; 1.2.4 Jet propulsion; 1.2.5 Industrial turbines; 1.2.6 Note on units; 2 Principles of Thermodynamics and Fluid Flow; 2.1 Mass conservation principle; 2.2 First law of thermodynamics.
Formatted contents note 2.3 Second law of thermodynamics2.3.1 Tds equations; 2.4 Equations of state; 2.4.1 Properties of steam; 2.4.2 Ideal gases; 2.4.3 Air tables and isentropic relations; 2.4.4 Ideal gas mixtures; 2.4.5 Incompressibility; 2.4.6 Stagnation state; 2.5 Efficiency; 2.5.1 Efficiency measures; 2.5.2 Thermodynamic losses; 2.5.3 Incompressible fluid; 2.5.4 Compressible flows; 2.6 Momentum balance; Exercises; 3 Compressible Flow through Nozzles; 3.1 Mach number and the speed of sound; 3.1.1 Mach number relations; 3.2 Isentropic flow with area change; 3.2.1 Converging nozzle.
Formatted contents note 3.2.2 Converging-diverging nozzle3.3 Normal shocks; 3.3.1 Rankine-Hugoniot relations; 3.4 Influence of friction in flow through straight nozzles; 3.4.1 Polytropic efficiency; 3.4.2 Loss coefficients; 3.4.3 Nozzle efficiency; 3.4.4 Combined Fanno flow and area change; 3.5 Supersaturation; 3.6 Prandtl-Meyer expansion; 3.6.1 Mach waves; 3.6.2 Prandtl-Meyer theory; 3.7 Flow leaving a turbine nozzle; Exercises; 4 Principles of Turbomachine Analysis; 4.1 Velocity triangles; 4.2 Moment of momentum balance; 4.3 Energy transfer in turbomachines; 4.3.1 Trothalpy and specific work in terms of velocities.
Formatted contents note 4.3.2 Degree of reaction4.4 Utilization; 4.5 Scaling and similitude; 4.5.1 Similitude; 4.5.2 Incompressible flow; 4.5.3 Shape parameter or specific speed; 4.5.4 Compressible flow analysis; 4.6 Performance characteristics; 4.6.1 Compressor performance map; 4.6.2 Turbine performance map; Exercises; 5 Steam Turbines; 5.1 Introduction; 5.2 Impulse turbines; 5.2.1 Single-stage impulse turbine; 5.2.2 Pressure compounding; 5.2.3 Blade shapes; 5.2.4 Velocity compounding; 5.3 Stage with zero reaction; 5.4 Loss coefficients; Exercises; 6 Axial Turbines; 6.1 Introduction; 6.2 Turbine stage analysis.
Formatted contents note 6.3 Flow and loading coefficients and reaction ratio6.3.1 Fifty percent (50%) stage; 6.3.2 Zero percent (0%) reaction stage; 6.3.3 Off-design operation; 6.4 Three-dimensional flow; 6.5 Radial equilibrium; 6.5.1 Free vortex flow; 6.5.2 Fixed blade angle; 6.6 Constant mass flux; 6.7 Turbine efficiency and losses; 6.7.1 Soderberg loss coefficients; 6.7.2 Stage efficiency; 6.7.3 Stagnation pressure losses; 6.7.4 Performance charts; 6.7.5 Zweifel correlation; 6.7.6 Further discussion of losses; 6.7.7 Ainley-Mathieson correlation; 6.7.8 Secondary loss; 6.8 Multistage turbine.
520 ## - SUMMARY, ETC.
Summary, etc The text is based on a course on turbomachinery which the author has taught since year 2000 as a technical elective. Topics include; Energy Transfer in Turbomachines, Gas and Steam Turbines, and Hydraulic Turbines. New material on wind turbines, and three-dimensional effects in axial turbomachines is included. The level is kept as such that students can smoothly move from a study of the most successful books in thermodynamics, fluid dynamics, and heat transfer to the subject of turbomachinery. The chapters are organized in such a way that the more difficult material is left to the later sectio.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name as entry element Turbomachines.
9 (RLIN) 28309
776 08 - ADDITIONAL PHYSICAL FORM ENTRY
Display text Print version:
Main entry heading Korpela, Seppo A.
Title Principles of Turbomachinery
Place, publisher, and date of publication Hoboken : John Wiley & Sons, c2011
International Standard Book Number 9780470536728.
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme
Item type Book
Copies
Price effective from Permanent location Date last seen Not for loan Date acquired Source of classification or shelving scheme Koha item type Barcode Damaged status Lost status Withdrawn status Current location Full call number
2014-07-14AUM Main Library2014-07-14 2014-07-14 BookAUM-019964   AUM Main Library621.406 K849
2014-07-14AUM Main Library2014-07-14 2014-07-14 BookAUM-019965   AUM Main Library621.406 K849