Hypersonic Slender Body Aerodynamics

Inbunden, Engelska, 2025

AvEthirajan Rathakrishnan,India) Rathakrishnan, Ethirajan (Indian Institute of Technology Kanpur

1 719 kr

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One-of-a-kind resource on theoretical and application aspects of hypersonic slender body aerodynamics with many didactic features included throughout Developed using class-tested course material, Hypersonic Slender Body Aerodynamics presents the theoretical and application aspects of the subject in a precise, concise, and student-friendly manner. The text includes a large number of worked examples, figures, diagrams, tables, and exercise problems. This book covers the subject material beginning from the definition of the slender body geometry through to the study of flow field around the body and the calculation of the aerodynamic and thermal loads acting on the body at speeds ranging from low to high (i.e., from incompressible to hypersonic speeds). The Mach number independence principle and approximate theories for caret wings are also covered, among many other key topics. This book is unique in its comprehensive coverage of the topic, enabling readers to find information in one place instead of scattered throughout proprietary wind tunnel test data, flight test data, government technical reports, scientific literature sources, and numerical methods. Some of the concepts explored in Hypersonic Slender Body Aerodynamics include: Wings of supersonic aircraft, covering sharp leading edges and ground and viscous effects, and pressure distribution on surfaces, covering transverse and longitudinal flowHypersonic aerodynamics, covering atmospheric properties, hypersonic-flow characteristics, governing equations, and flow past a semi-wedgeApplication of slender-body theory, covering leading-edge heat transfer, sublimation, aerodynamic effects, nose bluntness, blast-wave theory, and thin shock layersAxisymmetric slender bodies, covering potential flow solutions and pressure distribution, and drag of slender bodies, covering shape factor and blunt after-body correctionsSkillfully written with a clear and engaging writing style, Hypersonic Slender Body Aerodynamics is an essential learning resource on the subject for undergraduate and graduate students of aerospace engineering and practicing engineers working in aerospace research labs and industries. It is a perfect textbook for courses on slender body aerodynamics.

Produktinformation

Utgivningsdatum2025-02-21
Mått157 x 235 x 18 mm
Vikt558 g
FormatInbunden
SpråkEngelska
SerieAerospace Series
Antal sidor208
FörlagJohn Wiley & Sons Inc
ISBN9781394285631

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Ethirajan Rathakrishnan is a Professor in the Department of Aerospace Engineering and the founder of High Speed Jet Laboratory at the Indian Institute of Technology, Kanpur. His research interests focus on gas dynamics, including experimental and theoretical investigation, rarefied flows, applied gas dynamics and high speed jets, sudden expansion problems, aeroacoustics, and active and passive control of jets and base flows. He is the author of multiple books and has received numerous international awards.

Preface xiAbout the Author xiiiNomenclature xvAbout the Companion Website xix1 Basics11.1 Introduction 11.2 Supersonic Transport Aircraft 31.3 Wings of Supersonic Aircraft 41.4 Basic Equations 91.5 Pressure Distribution on the Surface 131.6 Theoretical Methods - Inviscid Flow 201.7 Stability Derivatives for Delta Wings 271.8 Method of Vortex (Source and Sink) Distribution 351.9 Cone in Supersonic Flow 451.10 Optimization (Supersonic Flow) 471.11 Lift-Case 511.12 Nonlinear Theories 551.13 Summary 592 Hypersonic Aerodynamics (Slender Bodies) 652.1 Introduction 652.2 Mach Number Independence Principle 682.3 Atmospheric Properties 702.4 Hypersonic Flow Characteristics 712.5 Governing Equations 722.6 Comparison of Supersonic and Hypersonic Flow 762.7 Re-entry Problem 792.8 Flow Past a Semi-wedge 802.9 Hypersonic Limiting Case 852.10 Newtonian Formula 862.11 Surface Pressure Distribution 882.12 Modified Newtonian Formula 892.13 Tangent Wedge or Tangent Cone Method 902.14 Busemann Correction for Centrifugal Force 902.15 Shock-Expansion Method 932.16 Theory of Slender Hypersonic Bodies 982.17 Principle of Equivalence for Slender Hypersonic Bodies 1022.18 Design of Three-Dimensional Hypersonic Slender Bodies 1042.19 Caret-Wing or Nonweiler Wing or Wave-Rider 1052.20 Off-design Conditions for Caret-Wings 1072.21 Approximate Theories for Caret-Wings 1082.22 Supersonic Test Facilities 1132.23 Comparison of Theoretical and Experimental Results 1202.24 Stability Derivatives 1212.25 Summary 1253 Application of Slender-body Theory 1333.1 Introduction 1333.2 Leading-Edge Heat Transfer 1363.3 Stagnation-Point Heat Transfer 1373.4 Heat Transfer Limitations for Slender-body Vehicles 1403.5 Sublimation 1433.6 Aerodynamic Effects 1433.7 Nose Bluntness 1443.8 Blast-wave Theory 1463.9 Thin Shock Layers 1483.10 Summary 1494 Experimental Approach 1554.1 Introduction 1554.2 Drag of Slender Bodies 1554.3 Axisymmetric Slender Bodies 1604.4 Summary 161Exercise Problems 163A Appendix 165References 171Further Readings 173Index 175

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