图书简介
New edition of the popular textbook, comprehensively updated throughout and now includes a new dedicated website for gas dynamic calculations The thoroughly revised and updated third edition of Fundamentals of Gas Dynamics maintains the focus on gas flows below hypersonic. This targeted approach provides a cohesive and rigorous examination of most practical engineering problems in this gas dynamics flow regime. The conventional one-dimensional flow approach together with the role of temperature-entropy diagrams are highlighted throughout. The authors-noted experts in the field-include a modern computational aid, illustrative charts and tables, and myriad examples of varying degrees of difficulty to aid in the understanding of the material presented. The updated edition of Fundamentals of Gas Dynamics includes new sections on the shock tube, the aerospike nozzle, and the gas dynamic laser. The book contains all equations, tables, and charts necessary to work the problems and exercises in each chapter. This book’s accessible but rigorous style: Offers a comprehensively updated edition that includes new problems and examples Covers fundamentals of gas flows targeting those below hypersonic Presents the one-dimensional flow approach and highlights the role of temperature-entropy diagrams Contains new sections that examine the shock tube, the aerospike nozzle, the gas dynamic laser, and an expanded coverage of rocket propulsion Explores applications of gas dynamics to aircraft and rocket engines Includes behavioral objectives, summaries, and check tests to aid with learning Written for students in mechanical and aerospace engineering and professionals and researchers in the field, the third edition of Fundamentals of Gas Dynamics has been updated to include recent developments in the field and retains all its learning aids. The calculator for gas dynamics calculations is available at https://www.oscarbiblarz.com/gascalculator gas dynamics calculations
Preface to Third Edition xi Preface to Second Edition xiii To the Student xv About the Companion Website xix 1 Definitions and Fundamental Principles 1 1.1 Introduction 1 1.2 Units and Notation 2 1.3 Why we use Nondimensional Quantities 8 1.4 Thermodynamic Concepts for Control Mass Analysis 12 Review Questions 21 Review Problems 24 2 Control Volume Analysis-Part I 27 2.1 Introduction 27 2.2 Objectives 28 2.3 Flow Dimensionality and Average Velocity 28 2.4 Transformation of a Material Derivative to a Control Volume Approach 31 2.5 Conservation of Mass 37 2.6 Conservation of Energy 39 2.7 Summary 48 Problems 50 Check Test 53 3 Control Volume Analysis-Part II 55 3.1 Introduction 55 3.2 Objectives 55 3.3 Comments on Entropy 56 3.4 Pressure-Energy Equation 58 3.5 The Stagnation Concept 60 3.6 Stagnation Pressure-Energy Equation 64 3.7 Consequences of Constant Density 66 3.8 Momentum Equation 71 3.9 Summary 80 Problems 82 Check Test 88 4 Introduction to Compressible Flow 91 4.1 Introduction 91 4.2 Objectives 92 4.3 Sonic Speed and Mach Number 92 4.4 Wave Propagation 98 4.5 Equations for Perfect Gases in Terms of Mach Number 100 4.6 h-s and T-s Diagrams 107 4.7 Summary 108 Problems 109 Check Test 112 5 Varying-Area Adiabatic Flow 115 5.1 Introduction 115 5.2 Objectives 116 5.3 General Fluid with No Losses 117 5.4 Perfect Gases with Losses 123 5.5 The Reference Concept 127 5.6 Isentropic Table 129 5.7 Nozzle Operation 136 5.8 Nozzle Performance 144 5.9 Diffuser Performance 146 5.10 When is not Equal to 1.4 148 5.11 Beyond the Tables 148 5.12 Summary 152 Problems 153 Check Test 157 6 Standing Normal Shocks 159 6.1 Introduction 159 6.2 Objectives 160 6.3 Shock Analysis: General Fluid 160 6.4 Working Equations for Perfect Gases 163 6.5 Normal-Shock Table 167 6.6 Shocks in Nozzles 172 6.7 Supersonic Wind Tunnel Operation 178 6.8 When is not Equal to 1.4 180 6.9 (Optional) Beyond the Tables 182 6.10 Summary 183 Problems 184 Check Test 188 7 Moving and Oblique Shocks 191 7.1 Introduction 191 7.2 Objectives 192 7.3 Normal Velocity Superposition: Moving Normal Shocks 192 7.4 Tangential Velocity Superposition: Oblique Shocks 196 7.5 Oblique-Shock Analysis: Perfect Gas 202 7.6 Oblique-Shock Table and Charts 204 7.7 Boundary Condition of Flow Direction 206 7.8 Boundary Condition of Pressure Equilibrium 210 7.9 Conical Shocks 213 7.10 The Shock Tube 216 7.11 (Optional) Beyond the Tables 219 7.12 Summary 221 Problems 222 Check Test 227 8 Prandtl-Meyer Flow 229 8.1 Introduction 229 8.2 Objectives 229 8.3 Argument for Isentropic Turning Flow 230 8.4 Analysis of Prandtl-Meyer Flow 237 8.5 Prandtl-Meyer Function 241 8.6 Overexpanded and Underexpanded Nozzles 244 8.7 Supersonic Airfoils 249 8.8 Aerospike Nozzle 254 8.9 When is not Equal to 1.4 256 8.10 (Optional) Beyond the Tables 257 8.11 Summary 258 Problems 259 Check Test 264 9 Fanno Flow 267 9.1 Introduction 267 9.2 Objectives 267 9.3 Analysis for a General Fluid 268 9.4 Working Equations for Perfect Gases 275 9.5 Reference State and Fanno Table 280 9.6 Applications 285 9.7 Correlation with Shocks 290 9.8 Friction Choking 292 9.9 (Optional) How the Left-Hand-Side of Equation (9.40) Arose 296 9.10 When is not Equal to 1.4 296 9.11 (Optional) Beyond the Tables 297 9.12 Summary 298 Problems 300 Check Test 305 10 Rayleigh Flow 307 10.1 Introduction 307 10.2 Objectives 308 10.3 Analysis for a General Fluid 309 10.4 Working Equations for Perfect Gases 319 10.5 Reference State and the Rayleigh Table 323 10.6 Applications 326 10.7 Correlation with Shocks 330 10.8 Thermal Choking Due to Heating 334 10.9 When is not Equal to 1.4 338 10.10 (Optional) Beyond the Tables 338 10.11 Summary 339 Problems 341 Check Test 347 11 Real Gas Effects 349 11.1 Introduction 349 11.2 Objectives 350 11.3 What’s Really Going on 351 11.4 Semiperfect Gas Behavior and Development of the Gas Tables 354 11.5 Real Gas Behavior, Equations of State and, Compressibility Factors 361 11.6 Variable- Variable-Area Flows 365 11.7 Variable- Constant-Area Flows 373 11.8 High-Energy Gas Lasers 375 11.9 Summary 377 Problems 380 Check Test 381 12 Propulsion Systems 383 12.1 Introduction 383 12.2 Objectives 384 12.3 Brayton Cycle 384 12.4 Propulsion Engines 394 12.5 General Performance Parameters, Thrust, Power, and Efficiency 412 12.6 Air-Breathing Propulsion Systems Performance Parameters 419 12.7 Air-Breathing Propulsion Systems Incorporating Real Gas Effects 424 12.8 Rocket Propulsion Systems Performance Parameters 426 12.9 Supersonic Diffusers 431 12.10 Summary 434 Problems 435 Check Test 439 Appendices A Summary of the English Engineering (EE) System of Units 441 B Summary of the International System (SI) of Units 445 C Friction-Factor Chart 449 D Oblique-Shock Charts ( = 1.4) (Two-Dimensional) 451 E Conical-Shock Charts ( = 1.4) (Three-Dimensional) 455 F Generalized Compressibility Factor Chart 459 G Isentropic Flow Parameters ( = 1.4) (Including Prandtl-Meyer Function) 461 H Normal-Shock Parameters ( = 1.4) 473 I Fanno Flow Parameters ( = 1.4) 483 J Rayleigh Flow Parameters ( = 1.4) 495 K Properties of Air at Low Pressure 507 L Specific Heats of Air at Low Pressures 517 Selected References 519 Answers to Problems 523 Index 535
Trade Policy 买家须知
- 关于产品：
- ● 正版保障：本网站隶属于中国国际图书贸易集团公司，确保所有图书都是100%正版。
- ● 环保纸张：进口图书大多使用的都是环保轻型张，颜色偏黄，重量比较轻。
- ● 毛边版：即书翻页的地方，故意做成了参差不齐的样子，一般为精装版，更具收藏价值。
关于退换货：- 由于预订产品的特殊性，采购订单正式发订后，买方不得无故取消全部或部分产品的订购。
- 由于进口图书的特殊性，发生以下情况的，请直接拒收货物，由快递返回：
- ● 外包装破损/发错货/少发货/图书外观破损/图书配件不全（例如：光盘等）
并请在工作日通过电话400-008-1110联系我们。
- 签收后，如发生以下情况，请在签收后的5个工作日内联系客服办理退换货：
- ● 缺页/错页/错印/脱线
关于发货时间：- 一般情况下：
- ●【现货】 下单后48小时内由北京（库房）发出快递。
- ●【预订】【预售】下单后国外发货，到货时间预计5-8周左右，店铺默认中通快递，如需顺丰快递邮费到付。
- ● 需要开具发票的客户，发货时间可能在上述基础上再延后1-2个工作日（紧急发票需求，请联系010-68433105/3213）；
- ● 如遇其他特殊原因，对发货时间有影响的，我们会第一时间在网站公告，敬请留意。
关于到货时间：- 由于进口图书入境入库后，都是委托第三方快递发货，所以我们只能保证在规定时间内发出，但无法为您保证确切的到货时间。
- ● 主要城市一般2-4天
- ● 偏远地区一般4-7天
关于接听咨询电话的时间：- 010-68433105/3213正常接听咨询电话的时间为：周一至周五上午8：30～下午5：00，周六、日及法定节假日休息，将无法接听来电，敬请谅解。
- 其它时间您也可以通过邮件联系我们：customer@readgo.cn,工作日会优先处理。
关于快递：- ● 已付款订单：主要由中通、宅急送负责派送，订单进度查询请拨打010-68433105/3213。
本书暂无推荐
本书暂无推荐
