LEADER 05208nam 2200601 450 001 9910463522403321 005 20200520144314.0 010 $a1-118-78757-9 010 $a1-118-78754-4 035 $a(CKB)2670000000570919 035 $a(EBL)1812458 035 $a(MiAaPQ)EBC1812458 035 $a(DLC) 2014022938 035 $a(Au-PeEL)EBL1812458 035 $a(CaPaEBR)ebr10951946 035 $a(CaONFJC)MIL650896 035 $a(OCoLC)892799668 035 $a(EXLCZ)992670000000570919 100 $a20141015h20152015 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $2rdacontent 182 $2rdamedia 183 $2rdacarrier 200 10$aTheoretical and computational aerodynamics /$fTapan K. Sengupta 210 1$aChichester, England :$cWiley,$d2015. 210 4$dİ2015 215 $a1 online resource (519 p.) 225 1 $aAerospace Series 300 $aDescription based upon print version of record. 311 $a1-118-78759-5 311 $a1-322-19616-8 320 $aIncludes bibliographical references at the end of each chapters and index. 327 $aTheoretical and Computational Aerodynamics; Contents; Series Preface; Preface; Acknowledgements; 1 Introduction to Aerodynamics and Atmosphere; 1.1 Motivation and Scope of Aerodynamics; 1.2 Conservation Principles; 1.2.1 Conservation Laws and Reynolds Transport Theorem (RTT); 1.2.2 Application of RTT: Conservation of Linear Momentum; 1.3 Origin of Aerodynamic Forces; 1.3.1 Momentum Integral Theory: Real Fluid Flow; 1.4 Flow in Accelerating Control Volumes: Application of RTT; 1.5 Atmosphere and Its Role in Aerodynamics; 1.5.1 Von Ka?rma?n Line; 1.5.2 Structure of Atmosphere 327 $a1.5.3 Armstrong Line or Limit1.5.4 International Standard Atmosphere (ISA) and Other Atmospheric Details; 1.5.5 Property Variations in Troposphere and Stratosphere; 1.6 Static Stability of Atmosphere; Bibliography; 2 Basic Equations of Motion; 2.1 Introduction; 2.1.1 Compressibility of Fluid Flow; 2.2 Conservation Principles; 2.2.1 Flow Description Method: Eulerian and Lagrangian Approaches; 2.2.2 The Continuity Equation: Mass Conservation; 2.3 Conservation of Linear Momentum: Integral Form; 2.4 Conservation of Linear Momentum: Differential Form 327 $a2.4.1 General Stress System in a Deformable Body2.5 Strain Rate of Fluid Element in Flows; 2.5.1 Kinematic Interpretation of Strain Tensor; 2.6 Relation between Stress and Rate of Strain Tensors in Fluid Flow; 2.7 Circulation and Rotationality in Flows; 2.8 Irrotational Flows and Velocity Potential; 2.9 Stream Function and Vector Potential; 2.10 Governing Equation for Irrotational Flows; 2.11 Kelvin's Theorem and Irrotationality; 2.12 Bernoulli's Equation: Relation of Pressure and Velocity; 2.13 Applications of Bernoulli's Equation: Air Speed Indicator; 2.13.1 Aircraft Speed Measurement 327 $a2.13.2 The Pressure Coefficient2.13.3 Compressibility Correction for Air Speed Indicator; 2.14 Viscous Effects and Boundary Layers; 2.15 Thermodynamics and Reynolds Transport Theorem; 2.16 Reynolds Transport Theorem; 2.17 The Energy Equation; 2.17.1 The Steady Flow Energy Equation; 2.18 Energy Conservation Equation; 2.19 Alternate Forms of Energy Equation; 2.20 The Energy Equation in Conservation Form; 2.21 Strong Conservation and Weak Conservation Forms; 2.22 Second Law of Thermodynamics and Entropy; 2.23 Propagation of Sound and Mach Number; 2.24 One-Dimensional Steady Flow 327 $a2.25 Normal Shock Relation for Steady Flow2.26 Rankine--Hugoniot Relation; 2.27 Prandtl or Meyer Relation; 2.28 Oblique ShockWaves; 2.29 Weak Oblique Shock; 2.30 Expansion of Supersonic Flows; Bibliography; 3 Theoretical Aerodynamics of Potential Flows; 3.1 Introduction; 3.2 Preliminaries of Complex Analysis for 2D Irrotational Flows: Cauchy--Riemann Relations; 3.2.1 Cauchy's Residue Theorem; 3.2.2 Complex Potential and Complex Velocity; 3.3 Elementary Singularities in Fluid Flows; 3.3.1 Superposing Solutions of Irrotational Flows; 3.4 Blasius' Theorem: Forces and Moment for Potential Flows 327 $a3.4.1 Force Acting on a Vortex in a Uniform Flow 330 $aTheoretical and Computational Aerodynamics is acomprehensive textbook covering classical aerodynamic theories and recent applications made possible by computational aerodynamics. Logically ordered for use in courses, the first seven chapters deal with classical methods of analysis up to the panel method and boundary layer solutions. The rest of the book is devoted to aspects of flow past aerodynamic surfaces from computational aspects to natural laminar flow (NLF) airfoils; transonic flows; flow control by active and passive devices. There is also a chapter devoted to low Reynolds number ae 410 0$aAerospace series (Chichester, England) 606 $aAerodynamics 608 $aElectronic books. 615 0$aAerodynamics. 676 $a629.132/3001 700 $aSengupta$b Tapan Kumar$f1955-$0478154 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910463522403321 996 $aTheoretical and computational aerodynamics$92016569 997 $aUNINA