{"product_id":"applied-gas-dynamics-isbn-9781119500452","title":"Applied Gas Dynamics","description":"\u003cp\u003e\u003cb\u003eA revised edition to applied gas dynamics with exclusive coverage on jets and additional sets of problems and examples\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003eThe revised and updated second edition of \u003ci\u003eApplied Gas Dynamics\u003c\/i\u003e offers an authoritative guide to the science of gas dynamics. Written by a noted expert on the topic, the text contains a comprehensive review of the topic; from a definition of the subject, to the three essential processes of this science: the isentropic process, shock and expansion process, and Fanno and Rayleigh flows.\u003c\/p\u003e \u003cp\u003eIn this revised edition, there are additional worked examples that highlight many concepts, including moving shocks, and a section on critical Mach number is included that helps to illuminate the concept. The second edition also contains new exercise problems with the answers added. In addition, the information on ram jets is expanded with helpful worked examples. It explores the entire spectrum of the ram jet theory and includes a set of exercise problems to aid in the understanding of the theory presented. This important text:\u003c\/p\u003e \u003cul\u003e \u003cli\u003eIncludes a wealth of new solved examples that describe the features involved in the design of gas dynamic devices \u003c\/li\u003e \u003cli\u003eContains a chapter on jets; this is the first textbook material available on high-speed jets\u003c\/li\u003e \u003cli\u003eOffers comprehensive and simultaneous coverage of both the theory and application\u003c\/li\u003e \u003cli\u003eIncludes additional information designed to help with an understanding of the material covered\u003c\/li\u003e \u003c\/ul\u003e \u003cp\u003eWritten for graduate students and advanced undergraduates in aerospace engineering and mechanical engineering,\u003ci\u003e Applied Gas Dynamics, Second Edition\u003c\/i\u003e expands on the original edition to include not only the basic information on the science of gas dynamics but also contains information on high-speed jets.\u003c\/p\u003e \u003cp\u003ePreface xv\u003c\/p\u003e \u003cp\u003eAuthor Biography xvii\u003c\/p\u003e \u003cp\u003eAbout the Companion Website xix\u003c\/p\u003e \u003cp\u003e\u003cb\u003e1 Basic Facts 1\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e1.1 Definition of Gas Dynamics 1\u003c\/p\u003e \u003cp\u003e1.2 Introduction 1\u003c\/p\u003e \u003cp\u003e1.3 Compressibility 2\u003c\/p\u003e \u003cp\u003e1.3.1 Limiting Conditions for Compressibility 3\u003c\/p\u003e \u003cp\u003e1.4 Supersonic Flow – What is it? 4\u003c\/p\u003e \u003cp\u003e1.5 Speed of Sound 5\u003c\/p\u003e \u003cp\u003e1.6 Temperature Rise 7\u003c\/p\u003e \u003cp\u003e1.7 Mach Angle 8\u003c\/p\u003e \u003cp\u003e1.7.1 Small Disturbance 10\u003c\/p\u003e \u003cp\u003e1.7.2 Finite Disturbance 10\u003c\/p\u003e \u003cp\u003e1.8 Thermodynamics of Fluid Flow 11\u003c\/p\u003e \u003cp\u003e1.9 First Law of Thermodynamics (Energy Equation) 11\u003c\/p\u003e \u003cp\u003e1.9.1 Energy Equation for an Open System 12\u003c\/p\u003e \u003cp\u003e1.9.2 Adiabatic Flow Process 14\u003c\/p\u003e \u003cp\u003e1.10 The Second Law of Thermodynamics (Entropy Equation) 15\u003c\/p\u003e \u003cp\u003e1.11 Thermal and Calorical Properties 16\u003c\/p\u003e \u003cp\u003e1.11.1 Thermally Perfect Gas 16\u003c\/p\u003e \u003cp\u003e1.12 The Perfect Gas 17\u003c\/p\u003e \u003cp\u003e1.12.1 Entropy Calculation 18\u003c\/p\u003e \u003cp\u003e1.12.2 Isentropic Relations 20\u003c\/p\u003e \u003cp\u003e1.12.3 Limitations on Air as a Perfect Gas 25\u003c\/p\u003e \u003cp\u003e1.13 Wave Propagation 26\u003c\/p\u003e \u003cp\u003e1.14 Velocity of Sound 26\u003c\/p\u003e \u003cp\u003e1.15 Subsonic and Supersonic Flows 27\u003c\/p\u003e \u003cp\u003e1.16 Similarity Parameters 28\u003c\/p\u003e \u003cp\u003e1.17 Continuum Hypothesis 28\u003c\/p\u003e \u003cp\u003e1.18 Compressible Flow Regimes 30\u003c\/p\u003e \u003cp\u003e1.19 Summary 31\u003c\/p\u003e \u003cp\u003eExercise Problems 34\u003c\/p\u003e \u003cp\u003e\u003cb\u003e2 Steady One-Dimensional Flow 43\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e2.1 Introduction 43\u003c\/p\u003e \u003cp\u003e2.2 Fundamental Equations 43\u003c\/p\u003e \u003cp\u003e2.3 Discharge from a Reservoir 45\u003c\/p\u003e \u003cp\u003e2.3.1 Mass Flow Rate per Unit Area 47\u003c\/p\u003e \u003cp\u003e2.3.2 Critical Values 51\u003c\/p\u003e \u003cp\u003e2.4 Streamtube Area–Velocity Relation 54\u003c\/p\u003e \u003cp\u003e2.5 de Laval Nozzle 57\u003c\/p\u003e \u003cp\u003e2.5.1 Mass Flow Relation in Terms of Mach Number 65\u003c\/p\u003e \u003cp\u003e2.5.2 Maximum Mass Flow Rate per Unit Area 65\u003c\/p\u003e \u003cp\u003e2.6 Supersonic Flow Generation 66\u003c\/p\u003e \u003cp\u003e2.6.1 Nozzles 68\u003c\/p\u003e \u003cp\u003e2.6.2 Physics of the Nozzle Flow Process 69\u003c\/p\u003e \u003cp\u003e2.7 Performance of Actual Nozzles 71\u003c\/p\u003e \u003cp\u003e2.7.1 Nozzle Efficiency 71\u003c\/p\u003e \u003cp\u003e2.7.2 Nozzle Discharge Coefficient 73\u003c\/p\u003e \u003cp\u003e2.8 Diffusers 75\u003c\/p\u003e \u003cp\u003e2.8.1 Special Features of Supersonic Diffusers 77\u003c\/p\u003e \u003cp\u003e2.8.2 Supersonic Wind Tunnel Diffusers 78\u003c\/p\u003e \u003cp\u003e2.8.3 Supersonic Inlets 81\u003c\/p\u003e \u003cp\u003e2.8.4 Fixed-Geometry Inlet 82\u003c\/p\u003e \u003cp\u003e2.8.5 Variable-Geometry Inlet 83\u003c\/p\u003e \u003cp\u003e2.8.6 Diffuser Efficiency 84\u003c\/p\u003e \u003cp\u003e2.9 Dynamic Head Measurement in Compressible Flow 88\u003c\/p\u003e \u003cp\u003e2.9.1 Compressibility Correction to Dynamic Pressure 91\u003c\/p\u003e \u003cp\u003e2.10 Pressure Coefficient 95\u003c\/p\u003e \u003cp\u003e2.11 Summary 97\u003c\/p\u003e \u003cp\u003eExercise Problems 99\u003c\/p\u003e \u003cp\u003e\u003cb\u003e3 Normal Shock Waves 113\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e3.1 Introduction 113\u003c\/p\u003e \u003cp\u003e3.2 Equations of Motion for a Normal Shock Wave 113\u003c\/p\u003e \u003cp\u003e3.3 The Normal Shock Relations for a Perfect Gas 115\u003c\/p\u003e \u003cp\u003e3.4 Change of Stagnation or Total Pressure Across a Shock 118\u003c\/p\u003e \u003cp\u003e3.5 Hugoniot Equation 121\u003c\/p\u003e \u003cp\u003e3.5.1 Moving Shocks 123\u003c\/p\u003e \u003cp\u003e3.6 The Propagating Shock Wave 123\u003c\/p\u003e \u003cp\u003e3.6.1 Weak Shock 128\u003c\/p\u003e \u003cp\u003e3.6.2 Strong Shock 130\u003c\/p\u003e \u003cp\u003e3.7 Reflected Shock Wave 133\u003c\/p\u003e \u003cp\u003e3.8 Centered Expansion Wave 138\u003c\/p\u003e \u003cp\u003e3.9 Shock Tube 139\u003c\/p\u003e \u003cp\u003e3.9.1 Shock Tube Applications 142\u003c\/p\u003e \u003cp\u003e3.10 Summary 145\u003c\/p\u003e \u003cp\u003eExercise Problems 148\u003c\/p\u003e \u003cp\u003e\u003cb\u003e4 Oblique Shock and Expansion Waves 155\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e4.1 Introduction 155\u003c\/p\u003e \u003cp\u003e4.2 Oblique Shock Relations 156\u003c\/p\u003e \u003cp\u003e4.3 Relation Between 𝛽 and 𝜃 158\u003c\/p\u003e \u003cp\u003e4.4 Shock Polar 160\u003c\/p\u003e \u003cp\u003e4.5 Supersonic Flow Over a Wedge 162\u003c\/p\u003e \u003cp\u003e4.6 Weak Oblique Shocks 165\u003c\/p\u003e \u003cp\u003e4.7 Supersonic Compression 167\u003c\/p\u003e \u003cp\u003e4.8 Supersonic Expansion by Turning 169\u003c\/p\u003e \u003cp\u003e4.9 The Prandtl–Meyer Expansion 170\u003c\/p\u003e \u003cp\u003e4.9.1 Velocity Components \u003ci\u003eV\u003csub\u003er\u003c\/sub\u003e\u003c\/i\u003e and \u003ci\u003eV\u003c\/i\u003e\u003ci\u003e\u003csub\u003e𝜙\u003c\/sub\u003e\u003c\/i\u003e 172\u003c\/p\u003e \u003cp\u003e4.9.2 The Prandtl–Meyer Function 175\u003c\/p\u003e \u003cp\u003e4.9.3 Compression 177\u003c\/p\u003e \u003cp\u003e4.10 Simple and Nonsimple Regions 178\u003c\/p\u003e \u003cp\u003e4.11 Reflection and Intersection of Shocks and Expansion Waves 178\u003c\/p\u003e \u003cp\u003e4.11.1 Intersection of Shocks of the Same Family 181\u003c\/p\u003e \u003cp\u003e4.11.2 Wave Reflection from a Free Boundary 183\u003c\/p\u003e \u003cp\u003e4.12 Detached Shocks 189\u003c\/p\u003e \u003cp\u003e4.13 Mach Reflection 191\u003c\/p\u003e \u003cp\u003e4.14 Shock-Expansion Theory 197\u003c\/p\u003e \u003cp\u003e4.15 Thin Airfoil Theory 202\u003c\/p\u003e \u003cp\u003e4.15.1 Application of Thin Aerofoil Theory 203\u003c\/p\u003e \u003cp\u003e4.16 Summary 210\u003c\/p\u003e \u003cp\u003eExercise Problems 212\u003c\/p\u003e \u003cp\u003e\u003cb\u003e5 Compressible Flow Equations 221\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e5.1 Introduction 221\u003c\/p\u003e \u003cp\u003e5.2 Crocco’s Theorem 221\u003c\/p\u003e \u003cp\u003e5.2.1 Basic Solutions of Laplace’s Equation 224\u003c\/p\u003e \u003cp\u003e5.3 General Potential Equation for Three-Dimensional Flow 225\u003c\/p\u003e \u003cp\u003e5.4 Linearization of the Potential Equation 226\u003c\/p\u003e \u003cp\u003e5.4.1 Small Perturbation Theory 227\u003c\/p\u003e \u003cp\u003e5.5 Potential Equation for Bodies of Revolution 229\u003c\/p\u003e \u003cp\u003e5.5.1 Conclusions 230\u003c\/p\u003e \u003cp\u003e5.5.2 Solution of Nonlinear Potential Equation 231\u003c\/p\u003e \u003cp\u003e5.6 Boundary Conditions 231\u003c\/p\u003e \u003cp\u003e5.6.1 Bodies of Revolution 232\u003c\/p\u003e \u003cp\u003e5.7 Pressure Coefficient 233\u003c\/p\u003e \u003cp\u003e5.7.1 Bodies of Revolution 234\u003c\/p\u003e \u003cp\u003e5.8 Summary 234\u003c\/p\u003e \u003cp\u003eExercise Problems 237\u003c\/p\u003e \u003cp\u003e\u003cb\u003e6 Similarity Rule 239\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e6.1 Introduction 239\u003c\/p\u003e \u003cp\u003e6.2 Two-Dimensional Flow: The Prandtl–Glauert Rule for Subsonic Flow 239\u003c\/p\u003e \u003cp\u003e6.2.1 Prandtl–Glauert Transformations 239\u003c\/p\u003e \u003cp\u003e6.2.2 The Direct Problem (Version I) 241\u003c\/p\u003e \u003cp\u003e6.2.3 The Indirect Problem (Case of Equal Potentials): P–G Transformation (Version II) 243\u003c\/p\u003e \u003cp\u003e6.2.4 Streamline Analogy (Version III): Gothert’s Rule 244\u003c\/p\u003e \u003cp\u003e6.3 Prandtl–Glauert Rule for Supersonic Flow: Versions I and II 245\u003c\/p\u003e \u003cp\u003e6.3.1 Subsonic Flow 246\u003c\/p\u003e \u003cp\u003e6.3.2 Supersonic Flow 246\u003c\/p\u003e \u003cp\u003e6.4 The von Karman Rule for Transonic Flow 248\u003c\/p\u003e \u003cp\u003e6.4.1 Use of the von Karman Rule 249\u003c\/p\u003e \u003cp\u003e6.5 Hypersonic Similarity 250\u003c\/p\u003e \u003cp\u003e6.6 Three-Dimensional Flow: Gothert’s Rule 252\u003c\/p\u003e \u003cp\u003e6.6.1 General Similarity Rule 252\u003c\/p\u003e \u003cp\u003e6.6.2 Gothert’s Rule 254\u003c\/p\u003e \u003cp\u003e6.6.3 Application toWings of Finite Span 255\u003c\/p\u003e \u003cp\u003e6.6.4 Application to Bodies of Revolution and Fuselages 255\u003c\/p\u003e \u003cp\u003e6.6.5 The Prandtl–Glauert Rule 257\u003c\/p\u003e \u003cp\u003e6.6.6 The von Karman Rule for Transonic Flow 261\u003c\/p\u003e \u003cp\u003e6.7 Critical Mach Number 261\u003c\/p\u003e \u003cp\u003e6.7.1 Calculation of M\u003csup\u003e∗\u003c\/sup\u003e\u003csub\u003e∞\u003c\/sub\u003e 264\u003c\/p\u003e \u003cp\u003e6.8 Summary 266\u003c\/p\u003e \u003cp\u003eExercise Problems 269\u003c\/p\u003e \u003cp\u003e\u003cb\u003e7 Two-Dimensional Compressible Flows 271\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e7.1 Introduction 271\u003c\/p\u003e \u003cp\u003e7.2 General Linear Solution for Supersonic Flow 271\u003c\/p\u003e \u003cp\u003e7.2.1 Existence of Characteristics in a Physical Problem 273\u003c\/p\u003e \u003cp\u003e7.2.2 Equation for the Streamlines from Kinematic Flow Condition 274\u003c\/p\u003e \u003cp\u003e7.3 Flow over a Wave-Shaped Wall 276\u003c\/p\u003e \u003cp\u003e7.3.1 Incompressible Flow 276\u003c\/p\u003e \u003cp\u003e7.3.2 Compressible Subsonic Flow 277\u003c\/p\u003e \u003cp\u003e7.3.3 Supersonic Flow 278\u003c\/p\u003e \u003cp\u003e7.3.4 Pressure Coefficient 278\u003c\/p\u003e \u003cp\u003e7.4 Summary 280\u003c\/p\u003e \u003cp\u003eExercise Problems 280\u003c\/p\u003e \u003cp\u003e\u003cb\u003e8 Flow with Friction and Heat Transfer 283\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e8.1 Introduction 283\u003c\/p\u003e \u003cp\u003e8.2 Flow in Constant Area Duct with Friction 283\u003c\/p\u003e \u003cp\u003e8.2.1 The Fanno Line 284\u003c\/p\u003e \u003cp\u003e8.3 Adiabatic, Constant-Area Flow of a Perfect Gas 285\u003c\/p\u003e \u003cp\u003e8.3.1 Definition of Friction Coefficient 286\u003c\/p\u003e \u003cp\u003e8.3.2 Effects of Wall Friction on Fluid Properties 287\u003c\/p\u003e \u003cp\u003e8.3.3 Second Law of Thermodynamics 288\u003c\/p\u003e \u003cp\u003e8.3.4 Working Relations 289\u003c\/p\u003e \u003cp\u003e8.4 Flow with Heating or Cooling in Ducts 294\u003c\/p\u003e \u003cp\u003e8.4.1 Governing Equations 294\u003c\/p\u003e \u003cp\u003e8.4.2 Simple-Heating Relations for a Perfect Gas 295\u003c\/p\u003e \u003cp\u003e8.5 Summary 300\u003c\/p\u003e \u003cp\u003eExercise Problems 303\u003c\/p\u003e \u003cp\u003e\u003cb\u003e9 Method of Characteristics 309\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e9.1 Introduction 309\u003c\/p\u003e \u003cp\u003e9.2 The Concepts of Characteristics 309\u003c\/p\u003e \u003cp\u003e9.3 The Compatibility Relation 310\u003c\/p\u003e \u003cp\u003e9.4 The Numerical Computational Method 312\u003c\/p\u003e \u003cp\u003e9.4.1 Solid and Free Boundary Points 313\u003c\/p\u003e \u003cp\u003e9.4.2 Sources of Error 316\u003c\/p\u003e \u003cp\u003e9.4.3 Axisymmetric Flow 316\u003c\/p\u003e \u003cp\u003e9.4.4 Nonisentropic Flow 317\u003c\/p\u003e \u003cp\u003e9.5 Theorems for Two-Dimensional Flow 318\u003c\/p\u003e \u003cp\u003e9.6 Numerical Computation with Weak Finite Waves 320\u003c\/p\u003e \u003cp\u003e9.6.1 Reflection of Waves 320\u003c\/p\u003e \u003cp\u003e9.7 Design of Supersonic Nozzle 323\u003c\/p\u003e \u003cp\u003e9.7.1 Contour Design Details 324\u003c\/p\u003e \u003cp\u003e9.8 Summary 328\u003c\/p\u003e \u003cp\u003e\u003cb\u003e10 Measurements in Compressible Flow 329\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e10.1 Introduction 329\u003c\/p\u003e \u003cp\u003e10.2 Pressure Measurements 329\u003c\/p\u003e \u003cp\u003e10.2.1 Liquid Manometers 329\u003c\/p\u003e \u003cp\u003e10.2.2 Measuring Principle of Manometers 330\u003c\/p\u003e \u003cp\u003e10.2.3 Dial-Type Pressure Gauges 332\u003c\/p\u003e \u003cp\u003e10.2.4 Pressure Transducers 333\u003c\/p\u003e \u003cp\u003e10.3 Temperature Measurements 335\u003c\/p\u003e \u003cp\u003e10.4 Velocity and Direction 338\u003c\/p\u003e \u003cp\u003e10.5 Density Problems 339\u003c\/p\u003e \u003cp\u003e10.6 Compressible Flow Visualization 339\u003c\/p\u003e \u003cp\u003e10.6.1 Supersonic Flows 340\u003c\/p\u003e \u003cp\u003e10.7 Interferometer 341\u003c\/p\u003e \u003cp\u003e10.7.1 Formation of Interference Patterns 341\u003c\/p\u003e \u003cp\u003e10.7.2 Quantitative Evaluation 342\u003c\/p\u003e \u003cp\u003e10.7.3 Fringe-Displacement Method 344\u003c\/p\u003e \u003cp\u003e10.8 Schlieren System 344\u003c\/p\u003e \u003cp\u003e10.8.1 Range and Sensitivity of the Schlieren System 347\u003c\/p\u003e \u003cp\u003e10.8.2 Optical Components Quality Requirements 347\u003c\/p\u003e \u003cp\u003e10.8.3 Sensitivity of the Schlieren Method for Shock and Expansion Studies 350\u003c\/p\u003e \u003cp\u003e10.9 Shadowgraph 352\u003c\/p\u003e \u003cp\u003e10.9.1 Comparison of the Schlieren and Shadowgraph Methods 353\u003c\/p\u003e \u003cp\u003e10.10 Wind Tunnels 354\u003c\/p\u003e \u003cp\u003e10.10.1 High-SpeedWind Tunnels 354\u003c\/p\u003e \u003cp\u003e10.10.2 Blowdown TypeWind Tunnels 354\u003c\/p\u003e \u003cp\u003e10.10.3 Induction Type Tunnels 355\u003c\/p\u003e \u003cp\u003e10.10.4 Continuous Supersonic Wind Tunnels 356\u003c\/p\u003e \u003cp\u003e10.10.5 Losses in Supersonic Tunnels 357\u003c\/p\u003e \u003cp\u003e10.10.6 Supersonic Wind Tunnel Diffusers 358\u003c\/p\u003e \u003cp\u003e10.10.7 Effects of Second Throat 360\u003c\/p\u003e \u003cp\u003e10.10.8 Compressor Tunnel Matching 362\u003c\/p\u003e \u003cp\u003e10.10.9 The Mass Flow Rate 365\u003c\/p\u003e \u003cp\u003e10.10.10 Blowdown Tunnel Operation 369\u003c\/p\u003e \u003cp\u003e10.10.11 Optimum Conditions 372\u003c\/p\u003e \u003cp\u003e10.10.12 Running Time of Blowdown Wind Tunnels 373\u003c\/p\u003e \u003cp\u003e10.11 Hypersonic Tunnels 375\u003c\/p\u003e \u003cp\u003e10.11.1 Hypersonic Nozzle 377\u003c\/p\u003e \u003cp\u003e10.12 Instrumentation and Calibration ofWind Tunnels 380\u003c\/p\u003e \u003cp\u003e10.12.1 Calibration of SupersonicWind Tunnels 380\u003c\/p\u003e \u003cp\u003e10.12.2 Calibration 381\u003c\/p\u003e \u003cp\u003e10.12.3 Mach Number Determination 381\u003c\/p\u003e \u003cp\u003e10.12.4 Pitot Pressure Measurement 382\u003c\/p\u003e \u003cp\u003e10.12.5 Static Pressure Measurement 382\u003c\/p\u003e \u003cp\u003e10.12.6 Determination of Flow Angularity 383\u003c\/p\u003e \u003cp\u003e10.12.7 Determination of Turbulence Level 383\u003c\/p\u003e \u003cp\u003e10.12.8 Determination of Test-Section Noise 384\u003c\/p\u003e \u003cp\u003e10.12.9 Use of Calibration Results 384\u003c\/p\u003e \u003cp\u003e10.12.10 Starting of Supersonic Tunnels 384\u003c\/p\u003e \u003cp\u003e10.12.11 Starting Loads 385\u003c\/p\u003e \u003cp\u003e10.12.12 Reynolds Number Effects 385\u003c\/p\u003e \u003cp\u003e10.12.13 Model Mounting-Sting Effects 385\u003c\/p\u003e \u003cp\u003e10.13 Calibration and Use of Hypersonic Tunnels 386\u003c\/p\u003e \u003cp\u003e10.13.1 Calibration of Hypersonic Tunnels 386\u003c\/p\u003e \u003cp\u003e10.13.2 Mach Number Determination 386\u003c\/p\u003e \u003cp\u003e10.13.3 Determination of Flow Angularity 388\u003c\/p\u003e \u003cp\u003e10.13.4 Determination of Turbulence Level 388\u003c\/p\u003e \u003cp\u003e10.13.5 Reynolds Number Effects 389\u003c\/p\u003e \u003cp\u003e10.13.6 Force Measurements 389\u003c\/p\u003e \u003cp\u003e10.14 Flow Visualization 390\u003c\/p\u003e \u003cp\u003e10.15 Summary 390\u003c\/p\u003e \u003cp\u003eExercise Problems 393\u003c\/p\u003e \u003cp\u003e\u003cb\u003e11 Ramjet 395\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e11.1 Introduction 395\u003c\/p\u003e \u003cp\u003e11.2 The Ideal Ramjet 396\u003c\/p\u003e \u003cp\u003e11.3 Aerodynamic Losses 401\u003c\/p\u003e \u003cp\u003e11.4 Aerothermodynamics of Engine Components 404\u003c\/p\u003e \u003cp\u003e11.4.1 Engine Inlets 404\u003c\/p\u003e \u003cp\u003e11.5 Flow Through Inlets 405\u003c\/p\u003e \u003cp\u003e11.5.1 Inlet Flow Process 406\u003c\/p\u003e \u003cp\u003e11.5.2 Boundary Layer Separation 406\u003c\/p\u003e \u003cp\u003e11.5.3 Flow Over the Inlet 406\u003c\/p\u003e \u003cp\u003e11.6 Performance of Actual Intakes 410\u003c\/p\u003e \u003cp\u003e11.6.1 Isentropic Efficiency 410\u003c\/p\u003e \u003cp\u003e11.6.2 Stagnation Pressure Ratio 411\u003c\/p\u003e \u003cp\u003e11.6.3 Supersonic Inlets 411\u003c\/p\u003e \u003cp\u003e11.6.4 Supersonic Diffusers 412\u003c\/p\u003e \u003cp\u003e11.6.5 Starting Problem 413\u003c\/p\u003e \u003cp\u003e11.7 Shock–Boundary Layer Interaction 418\u003c\/p\u003e \u003cp\u003e11.8 Oblique Shock Wave Incident on Flat Plate 419\u003c\/p\u003e \u003cp\u003e11.9 Normal Shocks in Ducts 420\u003c\/p\u003e \u003cp\u003e11.10 External Supersonic Compression 422\u003c\/p\u003e \u003cp\u003e11.11 Two-Shock Intakes 423\u003c\/p\u003e \u003cp\u003e11.12 Multi-Shock Intakes 427\u003c\/p\u003e \u003cp\u003e11.13 Isentropic Compression 429\u003c\/p\u003e \u003cp\u003e11.14 Limits of External Compression 431\u003c\/p\u003e \u003cp\u003e11.15 External Shock Attachment 433\u003c\/p\u003e \u003cp\u003e11.16 Internal Shock Attachment 433\u003c\/p\u003e \u003cp\u003e11.17 Pressure Loss 434\u003c\/p\u003e \u003cp\u003e11.18 Supersonic Combustion 442\u003c\/p\u003e \u003cp\u003e11.19 Summary 444\u003c\/p\u003e \u003cp\u003eExercise Problems 447\u003c\/p\u003e \u003cp\u003e\u003cb\u003e12 Jets 451\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e12.1 Introduction 451\u003c\/p\u003e \u003cp\u003e12.1.1 Subsonic Jets 453\u003c\/p\u003e \u003cp\u003e12.2 Mathematical Treatment of Jet Profiles 454\u003c\/p\u003e \u003cp\u003e12.3 Theory of Turbulent Jets 455\u003c\/p\u003e \u003cp\u003e12.3.1 Mean Velocity and Mean Temperature 456\u003c\/p\u003e \u003cp\u003e12.3.2 Turbulence Characteristics of Free Jets 457\u003c\/p\u003e \u003cp\u003e12.3.3 Mixing Length 458\u003c\/p\u003e \u003cp\u003e12.4 Experimental Methods for Studying Jets and the Techniques Used for Analysis 461\u003c\/p\u003e \u003cp\u003e12.4.1 Pressure Measurement 462\u003c\/p\u003e \u003cp\u003e12.5 Expansion Levels of Jets 464\u003c\/p\u003e \u003cp\u003e12.5.1 Overexpanded Jets 464\u003c\/p\u003e \u003cp\u003e12.5.2 Correctly Expanded Jets 467\u003c\/p\u003e \u003cp\u003e12.5.3 Underexpanded Jets 469\u003c\/p\u003e \u003cp\u003e12.6 Control of Jets 471\u003c\/p\u003e \u003cp\u003e12.6.1 Classification of Control Methods 473\u003c\/p\u003e \u003cp\u003e12.6.2 Role of Shear Layer in Flow Control 474\u003c\/p\u003e \u003cp\u003e12.6.3 Supersonic Shear Layers 475\u003c\/p\u003e \u003cp\u003e12.6.4 Use of Tabs for Jet Control 477\u003c\/p\u003e \u003cp\u003e12.6.5 Evaluation of the Effectiveness of Some Specific Passive Controls 481\u003c\/p\u003e \u003cp\u003e12.6.6 Grooves and Cutouts 519\u003c\/p\u003e \u003cp\u003e12.7 Noncircular Jets and Shifted Tabs 519\u003c\/p\u003e \u003cp\u003e12.7.1 Jet Control with Tabs 523\u003c\/p\u003e \u003cp\u003e12.7.2 Shifted Tabs 527\u003c\/p\u003e \u003cp\u003e12.7.3 Ventilated Triangular Tabs 532\u003c\/p\u003e \u003cp\u003e12.7.4 Tab Edge Effect 535\u003c\/p\u003e \u003cp\u003e12.8 Summary 541\u003c\/p\u003e \u003cp\u003eAppendix A 547\u003c\/p\u003e \u003cp\u003eReferences 619\u003c\/p\u003e \u003cp\u003eIndex 625\u003c\/p\u003e   \u003cp\u003e\u003cb\u003eETHIRAJAN RATHAKRISHNAN\u003c\/b\u003e is professor of Aerospace Engineering at the Indian Institute of Technology Kanpur, India. He is well known internationally for his research in the area of high-speed jets.    \u003c\/p\u003e\u003cp\u003e\u003cb\u003eA REVISED EDITION TO APPLIED GAS DYNAMICS WITH EXCLUSIVE COVERAGE ON JETS AND ADDITIONAL SETS OF PROBLEMS AND EXAMPLES\u003c\/b\u003e \u003c\/p\u003e\u003cp\u003eThe revised and updated second edition of \u003ci\u003eApplied Gas Dynamics\u003c\/i\u003e offers an authoritative guide to the science of gas dynamics. Written by a noted expert on the topic, the text contains a comprehensive review of the topic; from a definition of the subject, to the three essential processes of this science: the isentropic process, shock and expansion process, and Fanno and Rayleigh flows. \u003c\/p\u003e\u003cp\u003eIn this revised edition, there are additional worked examples that highlight many concepts, including moving shocks, and a section on critical Mach number is included that helps to illuminate the concept. The second edition also contains new exercise problems with the answers added. In addition, the information on ram jets is expanded with helpful worked examples. It explores the entire spectrum of the ram jet theory and includes a set of exercise problems to aid in the understanding of the theory presented. This important text: \u003c\/p\u003e\u003cul\u003e \u003cli\u003eIncludes a wealth of new solved examples that describe the features involved in the design of gas dynamic devices\u003c\/li\u003e \u003cli\u003eContains a chapter on jets; this is the first textbook material available on high-speed jets\u003c\/li\u003e \u003cli\u003eOffers comprehensive and simultaneous coverage of both the theory and application\u003c\/li\u003e \u003cli\u003eIncludes additional information designed to help with an understanding of the material covered\u003c\/li\u003e \u003c\/ul\u003e \u003cp\u003eWritten for graduate students and advanced undergraduates in aerospace engineering and mechanical engineering, \u003ci\u003eApplied Gas Dynamics, Second Edition\u003c\/i\u003e expands on the original edition to include not only the basic information on the science of gas dynamics but also contains information on high-speed jets.\u003c\/p\u003e","brand":"Wiley","offers":[{"title":"Default Title","offer_id":47988751139045,"sku":"NP9781119500452","price":116.0,"currency_code":"USD","in_stock":false}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/1842\/7735\/files\/9781119500452.jpg?v=1761781447","url":"https:\/\/k12savings.com\/products\/applied-gas-dynamics-isbn-9781119500452","provider":"K12savings","version":"1.0","type":"link"}