Verfügbarkeit: Introduction to flight

Introduction to flight:

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Bibliographische Detailangaben
1. Verfasser:	Anderson, John David 1937- (VerfasserIn)
Format:	Buch
Sprache:	English
Veröffentlicht:	Boston [u.a.] McGraw-Hill 2008
Ausgabe:	6. ed.
Schlagworte:	Aerodynamics Airplanes / Design and construction Space flight Airplanes > Design and construction Luftfahrttechnik Raumfahrt Raumfahrttechnik Flugzeugbau Aerodynamik Flugmechanik Lehrbuch
Online-Zugang:	Contributor biographical information lizenzfrei Inhaltsverzeichnis
Beschreibung:	XVI, 896 S. Ill., graph. Darst.
ISBN:	0073529397 9780073529394

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Datensatz im Suchindex

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adam_text	CONTENTS About the Author ¡ii Preface to the Sixth Edition xiii Preface to the First Edition xv Chapter 1 The First Aeronautical Engineers 1 1.1 Introduction 1 Very Early Developments 3 Sir George Cayley (1773-1857)— The True Inventor of the Airplane 6 The Interregnum — From 1853 to 1891 Otto Lilienthal (1848-1896)— The Glider Man 17 Percy Pilcher (1867-1899)— Extending the Glider Tradition 19 Aeronautics Comes to America 20 Wilbur (1867-1912) and Orville (1871-1948) Wright—Inventors of the First Practical Airplane 27 The Aeronautical Triangle — Langley, the Wrights, and Glenn Curtiss 36 1.10 The Problem of Propulsion 45 1.11 Faster and Higher 46 1.12 Summary 49 Bibliography 50 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 13 Chapter 2 Fundamental Thoughts 52 2.1 Fundamental Physical Quantities of a Flowing Gas 56 2. /. / Pressure 56 2.1.2 Density 57 2.1.3 Temperature 58 2.1.4 Flow Velocity and Streamlines 59 2.2 The Source of All Aerodynamic Forces 61 2.3 Equation of State for a Perfect Gas 63 2.4 Discussion of Units 65 2.5 Specific Volume 70 2.6 Anatomy of the Airplane 79 2.7 Anatomy of a Space Vehicle 89 2.8 Historical Note: The NACA and NASA 98 2.9 Summary 101 Bibliography 101 Problems 102 Chapter 3 The Standard Atmosphere 105 3.1 Definition of Altitude 107 3.2 Hydrostatic Equation 108 3.3 Relation between Geopotential and Geometric Altitudes 110 3.4 Definition of the Standard Atmosphere 111 3.5 Pressure, Temperature, and Density Altitudes 118 3.6 Historical Note: The Standard Atmosphere 121 3.7 Summary 123 Bibliography 124 Problems 124 vii viii Contents Ch apter 4 Basic Aerodynamics 126 4.1 Continuity Equation 130 4.2 Incompressible and Compressible How 131 4.3 Momentum Equation 134 4.4 A Comment 138 4.5 Elementary Thermodynamics 145 4.6 Isentropic Flow 151 4.7 Energy Equation 156 4.8 Summary of Equations 159 4.9 Speed of Sound 160 4.10 Low-Speed Subsonic Wind Tunnels 166 4.11 Measurement of Airspeed 172 4.11.1 Incompressible Flow 175 4.11.2 Subsonic Compressible Flow 178 4.11.3 Supersonic Flow 182 4.11.4 Summary 186 4.12 Some Additional Considerations 187 4.12.1 More about Compressible Flow 187 4.12.2 More about Equivalent Airspeed 189 4.13 Supersonic Wind Tunnels and Rocket Engines 191 4.14 Discussion of Compressibility 199 4.15 Introduction to Viscous Flow 200 4.16 Results for a Laminar Boundary Layer 209 4.17 Results for a Turbulent Boundary Layer 214 4.18 Compressibility Effects on Skin Friction 217 4.19 Transition 220 4.20 Flow Separation 223 4.21 Summary of Viscous Effects on Drag 228 4.22 Historical Note: Bernoulli and Euler 230 4.23 Historical Note: The Pitot Tube 231 4.24 Historical Note: The First Wind Tunnels 234 4.25 Historical Note: Osborne Reynolds and His Number 240 4.26 Historical Note: Prandtl and the Development of the Boundary Layer Concept 244 4.27 Summary 247 Bibliography 250 Problems 250 Chapter 5 Airfoils, Wings, and Other Aerodynamic Shapes 256 5.1 Introduction 256 5.2 Airfoil Nomenclature 258 5.3 Lift, Drag, and Moment Coefficients 262 5.4 Airfoil Data 268 5.5 Infinite Versus Finite Wings 279 5.6 Pressure Coefficient 280 5.7 Obtaining Lift Coefficient from Cp 286 5.8 Compressibility Correction for Lift Coefficient 290 5.9 Critical Mach Number and Critical Pressure Coefficient 291 5.10 Drag-Divergence Mach Number 303 5.11 Wave Drag (at Supersonic Speeds) 311 5.12 Summary of Airfoil Drag 319 5.13 Finite Wings 321 5.14 Calculation of Induced Drag 324 5.15 Change in the Lift Slope 332 5.16 Swept Wings 340 5.17 Flaps—A Mechanism for High Lift 353 5.18 Aerodynamics of Cylinders and Spheres 359 5.19 How Lift Is Produced — Some Alternative Explanations 363 5.20 Historical Note: Airfoils and Wings 373 5.20.1 The Wright Brothers 374 5.20.2 British and U.S. Airfoils (1910-1920) 374 Contents 5.20.3 1920-1930 375 5.20.4 Early NACA Four-Digit Airfoils 375 5.20.5 Later NACA Airfoils 376 5.20.6 Modern Airfoil Work 377 5.20.7 Finite Wings 377 5.21 Historical Note: Ernst Mach and His Number 380 5.22 Historical Note: The First Manned Supersonic Flight 383 5.23 Historical Note: The X-15 — First Manned Hypersonic Airplane and Stepping-Stone to the Space Shuttle 387 5.24 Summary 390 Bibliography 391 Problems 391 Chapter 6 Elements of Airplane Performance 396 6.1 Introduction: The Drag Polar 396 6.2 Equations of Motion 403 6.3 Thrust Required for Level, Unaccelerated Flight 405 6.4 Thrust Available and Maximum Velocity 413 6.5 Power Required for Level, Unaccelerated Flight 416 6.6 Power Available and Maximum Velocity 421 6.6.1 Reciprocating Engine-Propeller Combination 42 1 6.6.2 Jet Engine 424 6.7 Altitude Effects on Power Required and Available 425 6.8 Rate of Climb 430 6.9 Gliding Flight 439 6.10 Absolute and Service Ceilings 443 6.11 Time to Climb 446 6.12 Range and Endurance — Propeller-Driven Airplane 447 6.12.1 Physical Considerations 448 6.12.2 Quantitative Formulation 449 6.12.3 Breguet Formulas (Propeller-Driven Airplane) 451 6.13 Range and Endurance — Jet Airplane 455 6.13.1 Physical Considerations 456 6.13.2 Quantitative Formulation 457 6.14 Relations between CD о and CD , 461 6.15 Takeoff Performance 469 6.16 Landing Performance 475 6.17 Turning Flight and the V-n Diagram 479 6.18 Accelerated Rate of Climb (Energy Method) 486 6.19 Special Considerations for Supersonic Airplanes 493 6.20 Uninhabited Aerial Vehicles (UAVs) 497 6.21 A Philosophy of Conceptual Airplane Design 506 6.22 A Comment, and More about the Aspect Ratio 509 6.23 Historical Note: Drag Reduction — The NACA Cowling and the Fillet 509 6.24 Historical Note: Early Predictions of Airplane Performance 512 6.25 Historical Note: Breguet and the Range Formula 515 6.26 Historical Note: Aircraft Design — Evolution and Revolution 516 6.27 Summary 522 Bibliography 524 Problems 525 Chapter 7 Principles of Stability and Control 529 7.1 Introduction 529 7.2 Definition of Stability and Control 535 7.2.1 Static Stability 536 7.2.2 Dynamic Stability 537 7.2.3 Control 539 7.2.4 Partial Derivative 539 Contents 7.3 Moments on the Airplane 540 8.3 Lagrange s Equation 597 7.4 Absolute Angle of Attack 541 8.4 Orbit Equation 600 7.5 Criteria for Longitudinal Static 8.4.1 Force and Energy 600 Stability 543 8.4.2 Equation of Motion 602 7.6 Quantitative Discussion: Contribution of 8.5 Space Vehicle Trajectories — Some Basic the Wing to Mcg 548 Aspects 606 7.7 Contribution of the Tail to Mcg 552 8.6 Kepler s Laws 613 7.8 Total Pitching Moment about the Center of 8.7 The Vis-Viva (Energy) Equation 617 Gravity 555 8.8 Some Orbital Maneuvers 623 7.9 Equations for Longitudinal Static 8.8.1 Plane Changes 623 Stability 557 8.8.2 Orbital Transfers: Single-Impulse 7.10 Neutral Point 559 and Hohmann Transfers 628 7.11 Static Margin 560 8.9 Interplanetary Trajectories 636 7.12 Concept of Static Longitudinal 8.9.1 Hyperbolic Trajectories 637 Control 564 8.9.2 Sphere of Influence 639 7.13 Calculation of Elevator Angle to 8.9.3 Heliocentric Trajectories 639 Trim 569 8.9.4 Method of Patched Conies 640 7.14 Stick-Fixed versus Stick-Free Static 8.9.5 Gravity-Assist Trajectories 641 Stability 571 8.10 Lunar Transfer 648 7.15 Elevator Hinge Moment 572 8.11 Spacecraft Attitude Control 649 7.16 Stick-Free Longitudinal Static 8.12 Introduction to Earth and Planetary Stability 574 Entry 650 7.17 Directional Static Stability 578 8.13 Exponential Atmosphere 653 7.18 Lateral Static Stability 579 8.14 General Equations of Motion for 7.19 A Comment 581 Atmospheric Entry 653 7.20 Historical Note: The Wright Brothers 8.15 Application to Ballistic Entry 657 versus the European Philosophy of 8.16 Entry Heating 663 Stability and Control 582 8.17 Lifting Entry, with Application to the 7.21 Historical Note: The Development of Space Shuttle 670 Flight Controls 583 8.18 Historical Note: Kepler 674 7.22 Historical Note: The Tuck-Under 8.19 Historical Note: Newton and the Law Problem 585 of Gravitation 676 7.23 Summary 586 8.20 Historical Note: Lagrange 678 Bibliography 587 8.21 Historical Note: Unmanned Space Problems 587 Flight 678 Chapter 8 8.22 Historical Note: Manned Space Flight 683 Space Flight (Astronautics) 589 8.23 Summary 685 8.1 Introduction 589 Bibliography 687 8.2 Differential Equations 596 Problems 687 Contents xi Chapter 9 Propulsion 690 9.1 Introduction 690 9.2 Propeller 693 9.3 Reciprocating Engine 701 9.4 Jet Propulsion — The Thrust Equation 711 9.5 Turbojet Engine 714 9.5. / Thrust Buildup for a Turbojet Engine 719 9.6 Turbofan Engine 721 9.7 Ramjet Engine 724 9.8 Rocket Engine 728 9.9 Rocket Propellants — Some Considerations 735 9.9.1 Liquid Propellants 735 9.9.2 Solid Propellants 738 9.9.3 A Comment 740 9.10 Rocket Equation 741 9.11 Rocket Staging 742 9.12 Propellant Requirements for Spacecraft Trajectory Maneuvers 746 9.13 Electric Propulsion 749 9.13.1 Electron-Ion Thruster 750 9.13.2 Magnetoplasmadynamic Thruster 751 9.13.3 Arc-Jet Thruster 751 9.13.4 A Comment 751 9.14 Historical Note: Early Propeller Development 752 9.15 Historical Note: Early Development of the Internal Combustion Engine for Aviation 755 9.16 Historical Note: Inventors of Early Jet Engines 757 9.17 Historical Note: Early History of Rocket Engines 760 9.18 Summary 766 Bibliography 767 Problems 767 Chapter 10 Flight Vehicle Structures and Materials 770 10.1 Introduction 770 10.2 Some Physics of Solid Materials 771 10.2.1 Stress 771 10.2.2 Struin 773 10.2.3 Other Cases 774 10.2.4 Stress-Strain Diagram 775 10.3 Some Elements of an Aircraft Structure 778 10.3.1 Beams 781 10.3.2 Box Structures 786 10.4 Materials 789 10.5 Fatigue 793 10.6 Some Comments 794 10.7 Historical Note: Evolution of Flight Structures 794 Bibliography 805 Problems 806 Chapter 11 Hypersonic Vehicles 807 11.1 Introduction 807 11.2 Physical Aspects of Hypersonic Flow 811 11.2.1 Thin Shock Uiyers 811 11.2.2 Entropy Layer 812 11.2.3 Viscous Interaction 813 11.2.4 High-Temperature Effects 814 11.2.5 Urn-Density Flow 815 11.2.6 Recapitulation 819 11.3 Newtonian Law for Hypersonic Flow 819 11.4 Some Comments about Hypersonic Airplanes 825 11.5 Summary 834 Bibliography 834 Problems 834 xii Contents Appendix A Standard Atmosphere, Appendix D Airfoil Data 855 SIUnits 836 Index 884 Appendix В Standard Atmosphere, English Engineering Units 846 Appendix С Symbols and Conversion Factors 854
adam_txt	CONTENTS About the Author ¡ii Preface to the Sixth Edition xiii Preface to the First Edition xv Chapter 1 The First Aeronautical Engineers 1 1.1 Introduction 1 Very Early Developments 3 Sir George Cayley (1773-1857)— The True Inventor of the Airplane 6 The Interregnum — From 1853 to 1891 Otto Lilienthal (1848-1896)— The Glider Man 17 Percy Pilcher (1867-1899)— Extending the Glider Tradition 19 Aeronautics Comes to America 20 Wilbur (1867-1912) and Orville (1871-1948) Wright—Inventors of the First Practical Airplane 27 The Aeronautical Triangle — Langley, the Wrights, and Glenn Curtiss 36 1.10 The Problem of Propulsion 45 1.11 Faster and Higher 46 1.12 Summary 49 Bibliography 50 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 13 Chapter 2 Fundamental Thoughts 52 2.1 Fundamental Physical Quantities of a Flowing Gas 56 2. /. / Pressure 56 2.1.2 Density 57 2.1.3 Temperature 58 2.1.4 Flow Velocity and Streamlines 59 2.2 The Source of All Aerodynamic Forces 61 2.3 Equation of State for a Perfect Gas 63 2.4 Discussion of Units 65 2.5 Specific Volume 70 2.6 Anatomy of the Airplane 79 2.7 Anatomy of a Space Vehicle 89 2.8 Historical Note: The NACA and NASA 98 2.9 Summary 101 Bibliography 101 Problems 102 Chapter 3 The Standard Atmosphere 105 3.1 Definition of Altitude 107 3.2 Hydrostatic Equation 108 3.3 Relation between Geopotential and Geometric Altitudes 110 3.4 Definition of the Standard Atmosphere 111 3.5 Pressure, Temperature, and Density Altitudes 118 3.6 Historical Note: The Standard Atmosphere 121 3.7 Summary 123 Bibliography 124 Problems 124 vii viii Contents Ch apter 4 Basic Aerodynamics 126 4.1 Continuity Equation 130 4.2 Incompressible and Compressible How 131 4.3 Momentum Equation 134 4.4 A Comment 138 4.5 Elementary Thermodynamics 145 4.6 Isentropic Flow 151 4.7 Energy Equation 156 4.8 Summary of Equations 159 4.9 Speed of Sound 160 4.10 Low-Speed Subsonic Wind Tunnels 166 4.11 Measurement of Airspeed 172 4.11.1 Incompressible Flow 175 4.11.2 Subsonic Compressible Flow 178 4.11.3 Supersonic Flow 182 4.11.4 Summary 186 4.12 Some Additional Considerations 187 4.12.1 More about Compressible Flow 187 4.12.2 More about Equivalent Airspeed 189 4.13 Supersonic Wind Tunnels and Rocket Engines 191 4.14 Discussion of Compressibility 199 4.15 Introduction to Viscous Flow 200 4.16 Results for a Laminar Boundary Layer 209 4.17 Results for a Turbulent Boundary Layer 214 4.18 Compressibility Effects on Skin Friction 217 4.19 Transition 220 4.20 Flow Separation 223 4.21 Summary of Viscous Effects on Drag 228 4.22 Historical Note: Bernoulli and Euler 230 4.23 Historical Note: The Pitot Tube 231 4.24 Historical Note: The First Wind Tunnels 234 4.25 Historical Note: Osborne Reynolds and His Number 240 4.26 Historical Note: Prandtl and the Development of the Boundary Layer Concept 244 4.27 Summary 247 Bibliography 250 Problems 250 Chapter 5 Airfoils, Wings, and Other Aerodynamic Shapes 256 5.1 Introduction 256 5.2 Airfoil Nomenclature 258 5.3 Lift, Drag, and Moment Coefficients 262 5.4 Airfoil Data 268 5.5 Infinite Versus Finite Wings 279 5.6 Pressure Coefficient 280 5.7 Obtaining Lift Coefficient from Cp 286 5.8 Compressibility Correction for Lift Coefficient 290 5.9 Critical Mach Number and Critical Pressure Coefficient 291 5.10 Drag-Divergence Mach Number 303 5.11 Wave Drag (at Supersonic Speeds) 311 5.12 Summary of Airfoil Drag 319 5.13 Finite Wings 321 5.14 Calculation of Induced Drag 324 5.15 Change in the Lift Slope 332 5.16 Swept Wings 340 5.17 Flaps—A Mechanism for High Lift 353 5.18 Aerodynamics of Cylinders and Spheres 359 5.19 How Lift Is Produced — Some Alternative Explanations 363 5.20 Historical Note: Airfoils and Wings 373 5.20.1 The Wright Brothers 374 5.20.2 British and U.S. Airfoils (1910-1920) 374 Contents 5.20.3 1920-1930 375 5.20.4 Early NACA Four-Digit Airfoils 375 5.20.5 Later NACA Airfoils 376 5.20.6 Modern Airfoil Work 377 5.20.7 Finite Wings 377 5.21 Historical Note: Ernst Mach and His Number 380 5.22 Historical Note: The First Manned Supersonic Flight 383 5.23 Historical Note: The X-15 — First Manned Hypersonic Airplane and Stepping-Stone to the Space Shuttle 387 5.24 Summary 390 Bibliography 391 Problems 391 Chapter 6 Elements of Airplane Performance 396 6.1 Introduction: The Drag Polar 396 6.2 Equations of Motion 403 6.3 Thrust Required for Level, Unaccelerated Flight 405 6.4 Thrust Available and Maximum Velocity 413 6.5 Power Required for Level, Unaccelerated Flight 416 6.6 Power Available and Maximum Velocity 421 6.6.1 Reciprocating Engine-Propeller Combination 42 1 6.6.2 Jet Engine 424 6.7 Altitude Effects on Power Required and Available 425 6.8 Rate of Climb 430 6.9 Gliding Flight 439 6.10 Absolute and Service Ceilings 443 6.11 Time to Climb 446 6.12 Range and Endurance — Propeller-Driven Airplane 447 6.12.1 Physical Considerations 448 6.12.2 Quantitative Formulation 449 6.12.3 Breguet Formulas (Propeller-Driven Airplane) 451 6.13 Range and Endurance — Jet Airplane 455 6.13.1 Physical Considerations 456 6.13.2 Quantitative Formulation 457 6.14 Relations between CD о and CD , 461 6.15 Takeoff Performance 469 6.16 Landing Performance 475 6.17 Turning Flight and the V-n Diagram 479 6.18 Accelerated Rate of Climb (Energy Method) 486 6.19 Special Considerations for Supersonic Airplanes 493 6.20 Uninhabited Aerial Vehicles (UAVs) 497 6.21 A Philosophy of Conceptual Airplane Design 506 6.22 A Comment, and More about the Aspect Ratio 509 6.23 Historical Note: Drag Reduction — The NACA Cowling and the Fillet 509 6.24 Historical Note: Early Predictions of Airplane Performance 512 6.25 Historical Note: Breguet and the Range Formula 515 6.26 Historical Note: Aircraft Design — Evolution and Revolution 516 6.27 Summary 522 Bibliography 524 Problems 525 Chapter 7 Principles of Stability and Control 529 7.1 Introduction 529 7.2 Definition of Stability and Control 535 7.2.1 Static Stability 536 7.2.2 Dynamic Stability 537 7.2.3 Control 539 7.2.4 Partial Derivative 539 Contents 7.3 Moments on the Airplane 540 8.3 Lagrange' s Equation 597 7.4 Absolute Angle of Attack 541 8.4 Orbit Equation 600 7.5 Criteria for Longitudinal Static 8.4.1 Force and Energy 600 Stability 543 8.4.2 Equation of Motion 602 7.6 Quantitative Discussion: Contribution of 8.5 Space Vehicle Trajectories — Some Basic the Wing to Mcg 548 Aspects 606 7.7 Contribution of the Tail to Mcg 552 8.6 Kepler's Laws 613 7.8 Total Pitching Moment about the Center of 8.7 The Vis-Viva (Energy) Equation 617 Gravity 555 8.8 Some Orbital Maneuvers 623 7.9 Equations for Longitudinal Static 8.8.1 Plane Changes 623 Stability 557 8.8.2 Orbital Transfers: Single-Impulse 7.10 Neutral Point 559 and Hohmann Transfers 628 7.11 Static Margin 560 8.9 Interplanetary Trajectories 636 7.12 Concept of Static Longitudinal 8.9.1 Hyperbolic Trajectories 637 Control 564 8.9.2 Sphere of Influence 639 7.13 Calculation of Elevator Angle to 8.9.3 Heliocentric Trajectories 639 Trim 569 8.9.4 Method of Patched Conies 640 7.14 Stick-Fixed versus Stick-Free Static 8.9.5 Gravity-Assist Trajectories 641 Stability 571 8.10 Lunar Transfer 648 7.15 Elevator Hinge Moment 572 8.11 Spacecraft Attitude Control 649 7.16 Stick-Free Longitudinal Static 8.12 Introduction to Earth and Planetary Stability 574 Entry 650 7.17 Directional Static Stability 578 8.13 Exponential Atmosphere 653 7.18 Lateral Static Stability 579 8.14 General Equations of Motion for 7.19 A Comment 581 Atmospheric Entry 653 7.20 Historical Note: The Wright Brothers 8.15 Application to Ballistic Entry 657 versus the European Philosophy of 8.16 Entry Heating 663 Stability and Control 582 8.17 Lifting Entry, with Application to the 7.21 Historical Note: The Development of Space Shuttle 670 Flight Controls 583 8.18 Historical Note: Kepler 674 7.22 Historical Note: The "Tuck-Under" 8.19 Historical Note: Newton and the Law Problem 585 of Gravitation 676 7.23 Summary 586 8.20 Historical Note: Lagrange 678 Bibliography 587 8.21 Historical Note: Unmanned Space Problems 587 Flight 678 Chapter 8 8.22 Historical Note: Manned Space Flight 683 Space Flight (Astronautics) 589 8.23 Summary 685 8.1 Introduction 589 Bibliography 687 8.2 Differential Equations 596 Problems 687 Contents xi Chapter 9 Propulsion 690 9.1 Introduction 690 9.2 Propeller 693 9.3 Reciprocating Engine 701 9.4 Jet Propulsion — The Thrust Equation 711 9.5 Turbojet Engine 714 9.5. / Thrust Buildup for a Turbojet Engine 719 9.6 Turbofan Engine 721 9.7 Ramjet Engine 724 9.8 Rocket Engine 728 9.9 Rocket Propellants — Some Considerations 735 9.9.1 Liquid Propellants 735 9.9.2 Solid Propellants 738 9.9.3 A Comment 740 9.10 Rocket Equation 741 9.11 Rocket Staging 742 9.12 Propellant Requirements for Spacecraft Trajectory Maneuvers 746 9.13 Electric Propulsion 749 9.13.1 Electron-Ion Thruster 750 9.13.2 Magnetoplasmadynamic Thruster 751 9.13.3 Arc-Jet Thruster 751 9.13.4 A Comment 751 9.14 Historical Note: Early Propeller Development 752 9.15 Historical Note: Early Development of the Internal Combustion Engine for Aviation 755 9.16 Historical Note: Inventors of Early Jet Engines 757 9.17 Historical Note: Early History of Rocket Engines 760 9.18 Summary 766 Bibliography 767 Problems 767 Chapter 10 Flight Vehicle Structures and Materials 770 10.1 Introduction 770 10.2 Some Physics of Solid Materials 771 10.2.1 Stress 771 10.2.2 Struin 773 10.2.3 Other Cases 774 10.2.4 Stress-Strain Diagram 775 10.3 Some Elements of an Aircraft Structure 778 10.3.1 Beams 781 10.3.2 Box Structures 786 10.4 Materials 789 10.5 Fatigue 793 10.6 Some Comments 794 10.7 Historical Note: Evolution of Flight Structures 794 Bibliography 805 Problems 806 Chapter 11 Hypersonic Vehicles 807 11.1 Introduction 807 11.2 Physical Aspects of Hypersonic Flow 811 11.2.1 Thin Shock Uiyers 811 11.2.2 Entropy Layer 812 11.2.3 Viscous Interaction 813 11.2.4 High-Temperature Effects 814 11.2.5 Urn-Density Flow 815 11.2.6 Recapitulation 819 11.3 Newtonian Law for Hypersonic Flow 819 11.4 Some Comments about Hypersonic Airplanes 825 11.5 Summary 834 Bibliography 834 Problems 834 xii Contents Appendix A Standard Atmosphere, Appendix D Airfoil Data 855 SIUnits 836 Index 884 Appendix В Standard Atmosphere, English Engineering Units 846 Appendix С Symbols and Conversion Factors 854
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genre_facet	Lehrbuch
id	DE-604.BV035186066
illustrated	Illustrated
index_date	2024-07-02T22:59:44Z
indexdate	2024-07-09T21:26:58Z
institution	BVB
isbn	0073529397 9780073529394
language	English
lccn	2007028879
oai_aleph_id	oai:aleph.bib-bvb.de:BVB01-016992754
oclc_num	155715274
open_access_boolean
owner	DE-703 DE-29T DE-573
owner_facet	DE-703 DE-29T DE-573
physical	XVI, 896 S. Ill., graph. Darst.
publishDate	2008
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publisher	McGraw-Hill
record_format	marc
spelling	Anderson, John David 1937- Verfasser (DE-588)129741507 aut Introduction to flight John D. Anderson, Jr. 6. ed. Boston [u.a.] McGraw-Hill 2008 XVI, 896 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Aerodynamics Airplanes / Design and construction Space flight Airplanes Design and construction Luftfahrttechnik (DE-588)4168244-0 gnd rswk-swf Raumfahrt (DE-588)4048574-2 gnd rswk-swf Raumfahrttechnik (DE-588)4177061-4 gnd rswk-swf Flugzeugbau (DE-588)4154782-2 gnd rswk-swf Aerodynamik (DE-588)4000589-6 gnd rswk-swf Flugmechanik (DE-588)4154760-3 gnd rswk-swf (DE-588)4123623-3 Lehrbuch gnd-content Luftfahrttechnik (DE-588)4168244-0 s DE-604 Raumfahrttechnik (DE-588)4177061-4 s 1\p DE-604 Flugzeugbau (DE-588)4154782-2 s 2\p DE-604 Aerodynamik (DE-588)4000589-6 s 3\p DE-604 Flugmechanik (DE-588)4154760-3 s 4\p DE-604 Raumfahrt (DE-588)4048574-2 s 5\p DE-604 http://www.loc.gov/catdir/enhancements/fy0742/2007028879-b.html Contributor biographical information lizenzfrei http://www.loc.gov/catdir/enhancements/fy0742/2007028879-t.html lizenzfrei Inhaltsverzeichnis Digitalisierung UB Bayreuth application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016992754&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 2\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 3\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 4\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 5\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk
spellingShingle	Anderson, John David 1937- Introduction to flight Aerodynamics Airplanes / Design and construction Space flight Airplanes Design and construction Luftfahrttechnik (DE-588)4168244-0 gnd Raumfahrt (DE-588)4048574-2 gnd Raumfahrttechnik (DE-588)4177061-4 gnd Flugzeugbau (DE-588)4154782-2 gnd Aerodynamik (DE-588)4000589-6 gnd Flugmechanik (DE-588)4154760-3 gnd
subject_GND	(DE-588)4168244-0 (DE-588)4048574-2 (DE-588)4177061-4 (DE-588)4154782-2 (DE-588)4000589-6 (DE-588)4154760-3 (DE-588)4123623-3
title	Introduction to flight
title_auth	Introduction to flight
title_exact_search	Introduction to flight
title_exact_search_txtP	Introduction to flight
title_full	Introduction to flight John D. Anderson, Jr.
title_fullStr	Introduction to flight John D. Anderson, Jr.
title_full_unstemmed	Introduction to flight John D. Anderson, Jr.
title_short	Introduction to flight
title_sort	introduction to flight
topic	Aerodynamics Airplanes / Design and construction Space flight Airplanes Design and construction Luftfahrttechnik (DE-588)4168244-0 gnd Raumfahrt (DE-588)4048574-2 gnd Raumfahrttechnik (DE-588)4177061-4 gnd Flugzeugbau (DE-588)4154782-2 gnd Aerodynamik (DE-588)4000589-6 gnd Flugmechanik (DE-588)4154760-3 gnd
topic_facet	Aerodynamics Airplanes / Design and construction Space flight Airplanes Design and construction Luftfahrttechnik Raumfahrt Raumfahrttechnik Flugzeugbau Aerodynamik Flugmechanik Lehrbuch
url	http://www.loc.gov/catdir/enhancements/fy0742/2007028879-b.html http://www.loc.gov/catdir/enhancements/fy0742/2007028879-t.html http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016992754&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
work_keys_str_mv	AT andersonjohndavid introductiontoflight

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