LEADER 00850nam0-22003371i-450- 001 990001293440403321 010 $a0-536-01-090-0 035 $a000129344 035 $aFED01000129344 035 $a(Aleph)000129344FED01 035 $a000129344 100 $a20000920d1975----km-y0itay50------ba 101 0 $aeng 200 1 $aTopics in algebra$fI. N. Herstein 205 $a2nd ed. 210 $aLexington [MA]$cXerox College$dc1975 215 $axi, 388 p.$d24 cm 610 0 $aAlgebra 676 $a512 700 1$aHerstein,$bIsrael Nathan$f<1923-1988>$0327575 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990001293440403321 952 $a10-C-3$b18887$fMA1 959 $aMA1 962 $a12-01 962 $a13-01 962 $a20-01 996 $aTopics in algebra$927600 997 $aUNINA DB $aING01 LEADER 05291nam 2200601Ia 450 001 9910133597603321 005 20170810182527.0 010 $a1-299-18952-0 010 $a0-470-82501-4 010 $a0-470-82502-2 035 $a(CKB)3400000000000268 035 $a(EBL)818628 035 $a(OCoLC)817920643 035 $a(SSID)ssj0000506346 035 $a(PQKBManifestationID)11955283 035 $a(PQKBTitleCode)TC0000506346 035 $a(PQKBWorkID)10514706 035 $a(PQKB)10490032 035 $a(MiAaPQ)EBC818628 035 $a(EXLCZ)993400000000000268 100 $a20100115d2010 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aAerothermodynamics of turbomachinery$b[electronic resource] $eanalysis and design /$fNaixing Chen 210 $aSingapore ;$aHoboken, NJ $cJohn Wiley & Sons$dc2010 215 $a1 online resource (475 p.) 300 $aDescription based upon print version of record. 311 $a0-470-82500-6 320 $aIncludes bibliographical references and index. 327 $aAEROTHERMODYNAMICS OF TURBOMACHINERY: ANALYSIS AND DESIGN; Contents; Foreword; Preface; Acknowledgments; Nomenclature; 1 Introduction; 1.1 Introduction to the Study of the Aerothermodynamics of Turbomachinery; 1.2 Brief Description of the Development of the Numerical Study of the Aerothermodynamics of Turbomachinery; 1.3 Summary; Further Reading; 2 Governing Equations Expressed in Non-Orthogonal Curvilinear Coordinates to Calculate 3D Viscous Fluid Flow in Turbomachinery; 2.1 Introduction; 2.2 Aerothermodynamics Governing Equations (Navier-Stokes Equations) of Turbomachinery 327 $a2.3 Viscous and Heat Transfer Terms of Equations2.3.1 Viscous Stress Tensor; 2.3.2 Strain Tensor; 2.3.3 Viscous Force; 2.3.4 Rates of Work Done by the Viscous Stresses and Dissipation Function; 2.3.5 Heat Transfer Term; 2.4 Examples of Simplification of Viscous and Heat Transfer Terms; 2.4.1 Three-Dimensional Flow in Turbomachinery Expressed by Using Arbitrary Non-Orthogonal Coordinates; 2.4.2 S1 Stream-Surface Flow; 2.4.3 S2 Stream-Surface Flow; 2.4.4 Annulus Wall Boundary Layer; 2.4.5 Three-Dimensional Boundary Layer on Rotating Blade Surface; 2.5 Tensor Form of Governing Equations 327 $a2.5.1 Continuity Equation2.5.2 Momentum Equation; 2.5.3 Energy Equation; 2.5.4 Entropy Equation; 2.6 Integral Form of Governing Equations; 2.6.1 Continuity Equation; 2.6.2 Momentum Equation; 2.6.3 Energy Equation; 2.7 A Collection of the Basic Relationships for Non-Orthogonal Coordinates; 2.8 Summary; 3 Introduction to Boundary Layer Theory; 3.1 Introduction; 3.2 General Concepts of the Boundary Layer; 3.2.1 Nature of Boundary Layer Flow; 3.2.2 Boundary Layer Thicknesses; 3.2.3 Transition of the Boundary Layer Regime; 3.2.4 Boundary Layer Separation; 3.2.5 Thermal Boundary Layer; 3.3 Summary 327 $a4 Numerical Solutions of Boundary Layer Differential Equations4.1 Introduction; 4.2 Boundary Layer Equations Expressed in Partial Differential Form; 4.2.1 Two-Dimensional Laminar Boundary Layer Equations; 4.2.2 Laminar Boundary Layer Equations of Axisymmetrical Flow; 4.2.3 Turbulent Boundary Layer Equations; 4.2.4 Boundary Conditions of Solution; 4.3 Numerical Solution of the Boundary Layer Differential Equations for a Cascade on the Stream Surface of Revolution; 4.3.1 Boundary Layer Equations of S1 Stream Surface Flow of Revolution and Their Solution; 4.3.2 Turbulence Modeling 327 $a4.4 Calculation Results and Validations4.4.1 Laminar Boundary Layer Calculation Example; 4.4.2 Turbulent Boundary Layer with Favorable Pressure Gradient; 4.4.3 Turbulent Boundary Layer with Adverse Pressure Gradient (Ludweig and Tillmann); 4.4.4 Turbulent Boundary Layer with Favorable Pressure Gradient (Bell); 4.4.5 Turbulent Boundary Layer with Adverse Pressure Gradient (Schubauer and Spangenberg); 4.5 Application to Analysis of the Performance of Turbomachinery Blade Cascades; 4.5.1 Boundary Layer Momentum Thickness (Bammert's Experiment) 327 $a4.5.2 Laminar Boundary Layer Prediction (Turbine and Compressor Blade Profiles) 330 $aComputational Fluid Dynamics (CFD) is now an essential and effective tool used in the design of all types of turbomachine, and this topic constitutes the main theme of this book. With over 50 years of experience in the field of aerodynamics, Professor Naixing Chen has developed a wide range of numerical methods covering almost the entire spectrum of turbomachinery applications. Moreover, he has also made significant contributions to practical experiments and real-life designs. The book focuses on rigorous mathematical derivation of the equations governing flow and detailed descriptions of th 606 $aTurbomachines$xAerodynamics 606 $aTurbomachines$xDesign and construction 608 $aElectronic books. 615 0$aTurbomachines$xAerodynamics. 615 0$aTurbomachines$xDesign and construction. 676 $a621.406 700 $aChen$b Naixing$f1933-$0896606 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910133597603321 996 $aAerothermodynamics of turbomachinery$92003172 997 $aUNINA LEADER 00975nam a2200229 i 4500 001 991001229509707536 005 20020502185428.0 008 940104s1987 it ||| | ita 035 $ab11482448-39ule_inst 035 $aPRUMB57184$9ExL 040 $aScuola per assistenti sociali$bita 100 1 $aGarofalo, Diego$0258150 245 12$aL'intervento psicosociale di comunità per l'età evolutiva :$borientamenti ed esperienze su prevenzione, educazione sanitaria, handicap e scuola /$cDiego Garofalo 260 $aRoma :$bEISS,$c1987 300 $a37 p. ;$c24 cm. 490 0 $aProblemi sociali del nostro tempo ;$v28 907 $a.b11482448$b01-03-17$c01-07-02 912 $a991001229509707536 945 $aLE024 SS/C IV 9$g1$iLE024N-2538$lle021$nex DUSS$o-$pE0.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i11673412$z01-07-02 996 $aIntervento psicosociale di comunità per l'età evolutiva$9812475 997 $aUNISALENTO 998 $ale021$b01-01-94$cm$da $e-$fita$git $h2$i1