MARC Record from marc_columbia

LEADER: 08560cam a2200565 a 4500
001 12469841
005 20211030224143.0
006 m o d
007 cr cnu---unuuu
008 130502r20031984nyua ob 001 0 eng d
035 $a(OCoLC)ocn841493609
035 $a(NNC)12469841
040 $aVALIL$beng$epn$cVALIL$dOCLCF$dOCLCQ$dYDXCP$dOCLCQ$dUAB$dOCLCQ$dERL$dVLB$dDKU$dOCLCQ$dCEF$dRRP$dCOO$dOCLCQ$dZCU$dAU@$dOCLCQ$dERF$dOCLCQ$dMM9$dOCLCQ$dS2H$dOCLCO$dOCLCQ
019 $a1233051645
020 $a9780486317533$q(electronic bk.)
020 $a0486317536$q(electronic bk.)
020 $z0486428796
020 $z9780486428796
035 $a(OCoLC)841493609$z(OCoLC)1233051645
050 4 $aTL570$b.M587 2003eb
082 04 $a629.132/3$222
084 $aUF 4700$2rvk
084 $aMTA 390f$2stub
084 $aVER 505f$2stub
049 $aZCUA
100 1 $aMoran, Jack.
245 13 $aAn introduction to theoretical and computational aerodynamics /$cJack Moran.
260 $aMineola, N.Y. :$bDover Publications,$c2003.
300 $a1 online resource (xiii, 464 pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aDover Books on Aeronautical Engineering
504 $aIncludes bibliographical references and index.
588 0 $aPrint version record.
520 $aThis concise and highly readable introduction to theoretical and computational aerodynamics integrates both classical and modern developments, focusing on applying methods to actual wing design. Designed for a junior- or senior-level course and as a resource for practicing engineers, it features 221 figures. 1984 edition.
505 0 $aCover -- Title Page -- Copyright Page -- Dedication -- Preface -- Contents -- 1. Wings -- 1.1. Function -- 1.2. Geometry -- 1.3. References -- 1.4. Problems -- 2. Review of Basic Fluid Dynamics -- 2.1. Forces and Moments Due to Pressure -- 2.2. The Basic Conservation Laws of Fluid Mechanics -- 2.3. Vector Calculus -- 2.4. Differential Forms of the Conservation Laws -- 2.5. Rotational Velocity and Irrotational Flow -- 2.6. Two-Dimensional Incompressible Flow -- 2.6.1. Uniform Flow -- 2.6.2. Source Flow -- 2.6.3. Vortex Flow -- 2.7. Bibliography -- 2.8. Problems -- 3. Incompressible Irrotational Flow About Symmetric Airfoils at Zero Lift -- 3.1. Uniform Two-Dimensional Irrotational Incompressible Flow About an Isolated Body -- 3.2. Superposition of Fundamental Solutions -- 3.3. Dimensionless Variables -- 3.4. Rankine Ovals -- 3.5. Line Source Distributions -- 3.6. Flow Past Thin Symmetric Airfoils -- 3.7. Errors Near The Stagnation Points -- 3.8. Numerical Solution Based on Line Doublet Distributions -- 3.9. Relation of Numerical to Analytical Solutions -- 3.10. Complex-Variable Methods -- 3.10.1. Flow Past an Ellipse -- 3.10.2. Joukowsky Airfoils -- 3.11. Problems -- 3.12. Computer Programs -- 4. Lifting Airfoils in Incompressible Irrotational Flow -- 4.1. The Thin Airfoil: Thickness and Camber Problems -- 4.2. Forces and Moments on a Thin Airfoil -- 4.3. The Kutta Condition -- 4.4. Circulation Specification -- 4.5. The Cambered Thin Airfoil -- 4.6. Aerodynamics of The Thin Airfoil -- 4.7. The Lumped-Vortex Method -- 4.8. Panel Methods -- 4.8.1. Program Panel -- 4.9. Complex-Variables Methods -- 4.10. References -- 4.11. Problems -- 4.12. Computer Program -- 5. Wings of Finite Span -- 5.1. The Vortex System for a Thin Planar Wing of Finite Span -- 5.2. The Vortex-Lattice Method -- 5.3. Induced Drag -- 5.4. Lifting-Line Theory.
505 8 $a11.7. References -- 11.8. Problems -- 11.9. Computer Program -- Appendix A. An Important Integral -- Appendix B. The Integral -- Appendix C. Potential Flow Past a Corner -- Appendix D. Uniqueness of Solutions of Laplace Equation -- Appendix E. Fourier-Series Expansions -- Appendix F. Downwash Due to a Horseshoe Vortex -- Appendix G. Geometrical Demonstration That Strain is a Tensor -- Appendix H. Optimization of the SOR Method for the Laplace Equation -- Appendix I. Structure of a Weak Shock Wave -- Index.
505 8 $a5.5. The Elliptic Lift Distribution -- 5.6. The Optimal Wing -- 5.7. Nonelliptic Lift Distributions -- 5.8. References -- 5.9. Problems -- 5.10. Computer Program -- 6. The Navier-Stokes Equations -- 6.1. The Stress at a Point -- 6.2. Newton's Second Law For Fluids -- 6.3. Symmetry of Stresses -- 6.4. Molecular View of Stress in a Fluid -- 6.5. The No-Slip Condition -- 6.6. Unidirectional Flows -- 6.7. The Viscosity Coefficient -- 6.8. Pascal's Law -- 6.9. Strain Versus Rotation -- 6.10. Isotropy -- 6.11. Vectors and Tensors -- 6.12. The Stress Tensor -- 6.13. The Rate-of-Strain Tensor -- 6.14. The Two Coefficients of Viscosity -- 6.15. The Navier-Stokes Equations -- 6.16. Problems -- 7. The Boundary Layer -- 7.1. The Laminar Boundary Layer -- 7.2. Use of the Boundary-Layer Equations -- 7.2.1. Skin Friction -- 7.2.2. Displacement Thickness -- 7.2.3. Momentum Thickness -- 7.3. The Momentum Integral Equation -- 7.4. Velocity Profile Fitting: Laminar Boundary Layers -- 7.5. Thwaites's Method For Laminar Boundary Layers -- 7.6. Form Drag -- 7.7. Turbulent Flows -- 7.8. Velocity Profile Fitting: Turbulent Boundary Layers -- 7.9. Head's Method For Turbulent Boundary Layers -- 7.10. Transition From Laminar to Turbulent Flow -- 7.11. Boundary Layer Separation -- 7.12. Airfoil Performance Characteristics -- 7.13. The Development of Circulation About a Sharp-Tailed Airfoil -- 7.14. Computation of Boundary Layer Growth Along An Airfoil -- 7.15. References -- 7.16. Problems -- 7.17. Computer Program -- 8. Panel Methods -- 8.1. Mathematical Foundations: Green's Identity -- 8.2. Potential-Based Panel Methods -- 8.2.1. Constant-Potential Method -- 8.2.2. Linear-Potential Method -- 8.2.3. Equivalent Vortex Distributions -- 8.3. Vortex-Based Panel Methods -- 8.4. Source-Based Panel Methods -- 8.5. Comparisons of Source-, Doublet-, and Vortex-Based Methods.
505 8 $a8.6. References -- 8.7. Problems -- 9. Finite Difference Methods -- 9.1. Boundary-Value Problems in One Dimension -- 9.2. Convergence and Order of Accuracy -- 9.3. Incompressible Potential Flow Past a Thin Symmetric Airfoil -- 9.3.1. Direct Methods -- 9.3.2. Iterative Methods -- 9.4. Initial Problems: The Heat Equation -- 9.4.1. An Explicit Finite-Difference Method -- 9.4.2. Stability -- 9.4.3. Convergence -- 9.4.4. The Crank-Nicolson Method -- 9.4.5. Backward-Difference Schemes -- 9.5. References -- 9.6. Problems -- 9.7. Computer Programs -- 10. Finite-Difference Solution of the Boundary Layer Equations -- 10.1. Statement of The Problem -- 10.2. Similar Solutions of The Laminar Incompressible Boundary Layer -- 10.2.1. Finite-Difference Methods for the Falkner-Skan Equation -- 10.2.2. Iterative Solution of Nonlinear Equations -- 10.2.3. A Finite-Difference Method Based on a Second-Order Differential Equation -- 10.2.4. A Finite-Difference Method Based on a System of First-Order Equations -- 10.3. Transformation of The Laminar Boundary-Layer Equations For Arbitrary Pressure Gradients -- 10.3.1. Program Bdylay -- 10.4. Turbulent Boundary Layers -- 10.5. Separated Flows -- 10.6. References -- 10.7. Problems -- 10.8. Computer Programs -- 11. Compressible Potential Flow Past Airfoils -- 11.1. Shock Waves and Sound Waves -- 11.2. Equations of Compressible Steady Potential Flow -- 11.3. The Prandtl-Glauert Equation -- 11.4. Subsonic Flow Past Thin Airfoils -- 11.5. Supersonic Flow Past Thin Airfoils -- 11.6. Transonic Flow Past Thin Airfoils -- 11.6.1. Aerodynamics in the Transonic Range -- 11.6.2. Solution of the Transonic Small-Disturbance Equation: Subcriticai Flow -- 11.6.3. Conservative versus Nonconservative Difference Schemes -- 11.6.4. Supercritical Flow and Upwind Differencing -- 11.6.5. The Relaxation Iteration -- 11.6.6. The Poisson Iteration.
650 0 $aAerodynamics.
650 6 $aAérodynamique.
650 7 $aTECHNOLOGY & ENGINEERING$xAeronautics & Astronautics.$2bisacsh
650 7 $aAerodynamics.$2fast$0(OCoLC)fst00798195
650 7 $aAerodynamik$2gnd
655 4 $aElectronic books.
776 08 $iPrint version:$aMoran, Jack.$tIntroduction to theoretical and computational aerodynamics.$dMineola, N.Y. : Dover Publications, 2003$z0486428796$w(DLC) 2003043969$w(OCoLC)51804758
830 0 $aDover Books on Aeronautical Engineering.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio12469841$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS