Holdings: Introduction to flight

Introduction to flight:

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Bibliographic Details
Main Author:	Anderson, John David 1937- (Author)
Format:	Book
Language:	English
Published:	Boston McGraw-Hill 2008
Edition:	6. ed.
Subjects:	Aerodynamics Airplanes > Design and construction Space flight Flugzeugbau Flugmechanik Aerodynamik Raumfahrttechnik Raumfahrt Luftfahrttechnik Einführung
Online Access:	Beschreibung für Leser Contributor biographical information Publisher description Table of contents only Inhaltsverzeichnis
Item Description:	Includes bibliographical references and index
Physical Description:	XVI, 896 S. Ill., graph. Darst.
ISBN:	9780071263184

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adam_text	INTRODUCTION TO FLIGHT SIXTH EDITION JOHN D. ANDERSON, JR. CURATOR FOR AERODYNAMICS, NATIONAL AIR AND SPACE MUSEUM SMITHSONIAN INSTITUTION PROFESSOR EMERITUS UNIVERSITY OF MARYLAND BOSTON BURR RIDGE, IL DUBUQUE, IA MADISON, WL NEW YORK SAN FRANCISCO ST. LOUIS BANGKOK BOGOTA CARACAS KUALA LUMPUR LISBON LONDON MADRID MEXICO CITY MILAN MONTREAL NEW DELHI SANTIAGO SEOUL SINGAPORE SYDNEY TAIPEI TORONTO CONTENTS ABOUT THE AUTHOR III PREFACE TO THE SIXTH EDITION XIII PREFACE TO THE FIRST EDITION XV CHAPTER 1 THE FIRST AERONAUTICAL ENGINEERS 1 1.1 INTRODUCTION 1 1.2 VERY EARLY DEVELOPMENTS 3 1.3 SIR GEORGE CAYLEY (1773-1857)* THE TRUE INVENTOR OF THE AIRPLANE 6 1.4 THE INTERREGNUMFROM 1853 TO 1891 13 1.5 OTTO LILIENTHAL (1848-1896) THE GLIDER MAN 17 1.6 PERCY PILCHER (1867-1899)* EXTENDING THE GLIDER TRADITION 19 1.7 AERONAUTICS COMES TO AMERICA 20 1.8 WILBUR (1867-1912) AND ORVILLE (1871-1948) WRIGHTINVENTORS OF THE FIRST PRACTICAL AIRPLANE 27 1.9 THE AERONAUTICAL TRIANGLELANGLEY, THE WRIGHTS, AND GLENN CURTISS 36 1.10 TH E PROBLEM OF PROPULSION 45 1.11 FASTER AND HIGHER 46 1.12 SUMMARY 49 BIBLIOGRAPHY 50 CHAPTER 2 FUNDAMENTAL THOUGHTS 52 2.1 FUNDAMENTAL PHYSICAL QUANTITIES OF A FLOWING GAS 56 2.1.1 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 CHAPTER 4 BASIC AERODYNAMICS 126 4.1 CONTINUITY EQUATION 130 4.2 INCOMPRESSIBLE AND COMPRESSIBLE FLOW 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 C P 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 FLAPSA MECHANISM FOR HIGH LIFT 353 5.18 AERODYNAMICS OF CYLINDERS AND SPHERES 359 5.19 HOW LIFT IS PRODUCEDSOME 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 MODEM 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 HISTORICA L NOTE: THE X-15FIRST 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 421 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 ENDURANCEJET AIRPLANE 455 6.13.1 PHYSICAL CONSIDERATIONS 456 6.13.2 QUANTITATIVE FORMULATION 457 6.14 RELATIONS BETWEEN CP,O AND C D J 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 7.4 ABSOLUTE ANGLE OF ATTACK 541 7.5 CRITERIA FOR LONGITUDINAL STATIC STABILITY 543 7.6 QUANTITATIVE DISCUSSION: CONTRIBUTION OF THE WING TO M CG 548 7.7 CONTRIBUTION OF THE TAIL TO M CG 552 7.8 TOTAL PITCHING MOMENT ABOUT THE CENTER OF GRAVITY 555 7.9 EQUATIONS FOR LONGITUDINAL STATIC STABILITY 557 7.10 NEUTRAL POINT 559 7.11 STATIC MARGIN 560 7.12 CONCEPT OF STATIC LONGITUDINAL CONTROL 564 7.13 CALCULATION OF ELEVATOR ANGLE TO TRIM 569 7.14 STICK-FIXED VERSUS STICK-FREE STATIC STABILITY 571 7.15 ELEVATOR HINGE MOMENT 572 7.16 STICK-FREE LONGITUDINAL STATIC STABILITY 574 7.17 DIRECTIONAL STATIC STABILITY 578 7.18 LATERAL STATIC STABILITY 579 7.19 A COMMENT 581 7.20 HISTORICAL NOTE: THE WRIGHT BROTHERS VERSUS THE EUROPEAN PHILOSOPHY OF STABILITY AND CONTROL 582 7.21 HISTORICAL NOTE: THE DEVELOPMENT OF FLIGHT CONTROLS 583 7.22 HISTORICAL NOTE: THE TUCK-UNDER PROBLEM 585 7.23 SUMMARY 586 BIBLIOGRAPHY 587 PROBLEMS 587 CHAPTER 8 SPACE FLIGHT (ASTRONAUTICS) 589 8.1 INTRODUCTION 589 8.2 DIFFERENTIAL EQUATIONS 596 8.3 LAGRANGE S EQUATION 597 8.4 ORBIT EQUATION 600 8.4.1 FORCE AND ENERGY 600 8.4.2 EQUATION OF MOTION 602 8.5 SPACE VEHICLE TRAJECTORIESSOME BASIC ASPECTS 606 8.6 KEPLER S LAWS 613 8.7 THE VIS-VIVA (ENERGY) EQUATION 617 8.8 SOME ORBITAL MANEUVERS 623 8.8.1 PLANE CHANGES 623 8.8.2 ORBITAL TRANSFERS: SINGLE-IMPULSE AND HOHMANN TRANSFERS 628 8.9 INTERPLANETARY TRAJECTORIES 636 8.9.1 HYPERBOLIC TRAJECTORIES 637 8.9.2 SPHERE OF INFLUENCE 639 8.9.3 HELIOCENTRIC TRAJECTORIES 639 8.9.4 METHOD OF PATCHED CONIES 640 8.9.5 GRAVITY-ASSIST TRAJECTORIES 641 8.10 LUNAR TRANSFER 648 8.11 SPACECRAFT ATTITUDE CONTROL 649 8.12 INTRODUCTION TO EARTH AND PLANETARY ENTRY 650 8.13 EXPONENTIAL ATMOSPHERE 653 8.14 GENERAL EQUATIONS OF MOTION FOR ATMOSPHERIC ENTRY 653 8.15 APPLICATION TO BALLISTIC ENTRY 657 8.16 ENTRY HEATING 663 8.17 LIFTING ENTRY, WITH APPLICATION TO THE SPACE SHUTTLE 670 8.18 HISTORICAL NOTE: KEPLER 674 8.19 HISTORICAL NOTE: NEWTON AND THE LAW OF GRAVITATION 676 8.20 HISTORICAL NOTE: LAGRANGE 678 8.21 HISTORICAL NOTE: UNMANNED SPACE FLIGHT 678 8.22 HISTORICAL NOTE: MANNED SPACE FLIGHT 683 8.23 SUMMARY 685 BIBLIOGRAPHY 687 PROBLEMS 687 CONTENTS XI CHAPTER 9 PROPULSION 690 9.1 INTRODUCTION 690 9.2 PROPELLER 693 9.3 RECIPROCATING ENGINE 701 9.4 JET PROPULSIONTHE THRUST EQUATION 711 9.5 TURBOJET ENGINE 714 9.5.7 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 9.9.7 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 70.2.7 STRESS 771 10.2.2 STRAIN 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 77.2.7 THIN SHOCK LAYERS 811 11.2.2 ENTROPY LAYER 812 11.2.3 VISCOUS INTERACTION 813 11.2.4 HIGH-TEMPERATURE EFFECTS 814 11.2.5 LOW-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 SI UNITS 836 T , QQA INDEX 884 APPENDIX B STANDARD ATMOSPHERE, ENGLISH ENGINEERING UNITS 846 APPENDIX C SYMBOLS AND CONVERSION FACTORS 854
adam_txt	INTRODUCTION TO FLIGHT SIXTH EDITION JOHN D. ANDERSON, JR. CURATOR FOR AERODYNAMICS, NATIONAL AIR AND SPACE MUSEUM SMITHSONIAN INSTITUTION PROFESSOR EMERITUS UNIVERSITY OF MARYLAND BOSTON BURR RIDGE, IL DUBUQUE, IA MADISON, WL NEW YORK SAN FRANCISCO ST. LOUIS BANGKOK BOGOTA CARACAS KUALA LUMPUR LISBON LONDON MADRID MEXICO CITY MILAN MONTREAL NEW DELHI SANTIAGO SEOUL SINGAPORE SYDNEY TAIPEI TORONTO CONTENTS ABOUT THE AUTHOR III PREFACE TO THE SIXTH EDITION XIII PREFACE TO THE FIRST EDITION XV CHAPTER 1 THE FIRST AERONAUTICAL ENGINEERS 1 1.1 INTRODUCTION 1 1.2 VERY EARLY DEVELOPMENTS 3 1.3 SIR GEORGE CAYLEY (1773-1857)* THE TRUE INVENTOR OF THE AIRPLANE 6 1.4 THE INTERREGNUMFROM 1853 TO 1891 13 1.5 OTTO LILIENTHAL (1848-1896) THE GLIDER MAN 17 1.6 PERCY PILCHER (1867-1899)* EXTENDING THE GLIDER TRADITION 19 1.7 AERONAUTICS COMES TO AMERICA 20 1.8 WILBUR (1867-1912) AND ORVILLE (1871-1948) WRIGHTINVENTORS OF THE FIRST PRACTICAL AIRPLANE 27 1.9 THE AERONAUTICAL TRIANGLELANGLEY, THE WRIGHTS, AND GLENN CURTISS 36 1.10 TH E PROBLEM OF PROPULSION 45 1.11 FASTER AND HIGHER 46 1.12 SUMMARY 49 BIBLIOGRAPHY 50 CHAPTER 2 FUNDAMENTAL THOUGHTS 52 2.1 FUNDAMENTAL PHYSICAL QUANTITIES OF A FLOWING GAS 56 2.1.1 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 CHAPTER 4 BASIC AERODYNAMICS 126 4.1 CONTINUITY EQUATION 130 4.2 INCOMPRESSIBLE AND COMPRESSIBLE FLOW 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 C P 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 FLAPSA MECHANISM FOR HIGH LIFT 353 5.18 AERODYNAMICS OF CYLINDERS AND SPHERES 359 5.19 HOW LIFT IS PRODUCEDSOME 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 MODEM 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 HISTORICA L NOTE: THE X-15FIRST 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 421 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 ENDURANCEJET AIRPLANE 455 6.13.1 PHYSICAL CONSIDERATIONS 456 6.13.2 QUANTITATIVE FORMULATION 457 6.14 RELATIONS BETWEEN CP,O AND C D J 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 7.4 ABSOLUTE ANGLE OF ATTACK 541 7.5 CRITERIA FOR LONGITUDINAL STATIC STABILITY 543 7.6 QUANTITATIVE DISCUSSION: CONTRIBUTION OF THE WING TO M CG 548 7.7 CONTRIBUTION OF THE TAIL TO M CG 552 7.8 TOTAL PITCHING MOMENT ABOUT THE CENTER OF GRAVITY 555 7.9 EQUATIONS FOR LONGITUDINAL STATIC STABILITY 557 7.10 NEUTRAL POINT 559 7.11 STATIC MARGIN 560 7.12 CONCEPT OF STATIC LONGITUDINAL CONTROL 564 7.13 CALCULATION OF ELEVATOR ANGLE TO TRIM 569 7.14 STICK-FIXED VERSUS STICK-FREE STATIC STABILITY 571 7.15 ELEVATOR HINGE MOMENT 572 7.16 STICK-FREE LONGITUDINAL STATIC STABILITY 574 7.17 DIRECTIONAL STATIC STABILITY 578 7.18 LATERAL STATIC STABILITY 579 7.19 A COMMENT 581 7.20 HISTORICAL NOTE: THE WRIGHT BROTHERS VERSUS THE EUROPEAN PHILOSOPHY OF STABILITY AND CONTROL 582 7.21 HISTORICAL NOTE: THE DEVELOPMENT OF FLIGHT CONTROLS 583 7.22 HISTORICAL NOTE: THE "TUCK-UNDER" PROBLEM 585 7.23 SUMMARY 586 BIBLIOGRAPHY 587 PROBLEMS 587 CHAPTER 8 SPACE FLIGHT (ASTRONAUTICS) 589 8.1 INTRODUCTION 589 8.2 DIFFERENTIAL EQUATIONS 596 8.3 LAGRANGE'S EQUATION 597 8.4 ORBIT EQUATION 600 8.4.1 FORCE AND ENERGY 600 8.4.2 EQUATION OF MOTION 602 8.5 SPACE VEHICLE TRAJECTORIESSOME BASIC ASPECTS 606 8.6 KEPLER'S LAWS 613 8.7 THE VIS-VIVA (ENERGY) EQUATION 617 8.8 SOME ORBITAL MANEUVERS 623 8.8.1 PLANE CHANGES 623 8.8.2 ORBITAL TRANSFERS: SINGLE-IMPULSE AND HOHMANN TRANSFERS 628 8.9 INTERPLANETARY TRAJECTORIES 636 8.9.1 HYPERBOLIC TRAJECTORIES 637 8.9.2 SPHERE OF INFLUENCE 639 8.9.3 HELIOCENTRIC TRAJECTORIES 639 8.9.4 METHOD OF PATCHED CONIES 640 8.9.5 GRAVITY-ASSIST TRAJECTORIES 641 8.10 LUNAR TRANSFER 648 8.11 SPACECRAFT ATTITUDE CONTROL 649 8.12 INTRODUCTION TO EARTH AND PLANETARY ENTRY 650 8.13 EXPONENTIAL ATMOSPHERE 653 8.14 GENERAL EQUATIONS OF MOTION FOR ATMOSPHERIC ENTRY 653 8.15 APPLICATION TO BALLISTIC ENTRY 657 8.16 ENTRY HEATING 663 8.17 LIFTING ENTRY, WITH APPLICATION TO THE SPACE SHUTTLE 670 8.18 HISTORICAL NOTE: KEPLER 674 8.19 HISTORICAL NOTE: NEWTON AND THE LAW OF GRAVITATION 676 8.20 HISTORICAL NOTE: LAGRANGE 678 8.21 HISTORICAL NOTE: UNMANNED SPACE FLIGHT 678 8.22 HISTORICAL NOTE: MANNED SPACE FLIGHT 683 8.23 SUMMARY 685 BIBLIOGRAPHY 687 PROBLEMS 687 CONTENTS XI CHAPTER 9 PROPULSION 690 9.1 INTRODUCTION 690 9.2 PROPELLER 693 9.3 RECIPROCATING ENGINE 701 9.4 JET PROPULSIONTHE THRUST EQUATION 711 9.5 TURBOJET ENGINE 714 9.5.7 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 9.9.7 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 70.2.7 STRESS 771 10.2.2 STRAIN 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 77.2.7 THIN SHOCK LAYERS 811 11.2.2 ENTROPY LAYER 812 11.2.3 VISCOUS INTERACTION 813 11.2.4 HIGH-TEMPERATURE EFFECTS 814 11.2.5 LOW-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 SI UNITS 836 T , QQA INDEX 884 APPENDIX B STANDARD ATMOSPHERE, ENGLISH ENGINEERING UNITS 846 APPENDIX C SYMBOLS AND CONVERSION FACTORS 854
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spellingShingle	Anderson, John David 1937- Introduction to flight Aerodynamics Airplanes Design and construction Space flight Flugzeugbau (DE-588)4154782-2 gnd Flugmechanik (DE-588)4154760-3 gnd Aerodynamik (DE-588)4000589-6 gnd Raumfahrttechnik (DE-588)4177061-4 gnd Raumfahrt (DE-588)4048574-2 gnd Luftfahrttechnik (DE-588)4168244-0 gnd
subject_GND	(DE-588)4154782-2 (DE-588)4154760-3 (DE-588)4000589-6 (DE-588)4177061-4 (DE-588)4048574-2 (DE-588)4168244-0 (DE-588)4151278-9
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 Flugzeugbau (DE-588)4154782-2 gnd Flugmechanik (DE-588)4154760-3 gnd Aerodynamik (DE-588)4000589-6 gnd Raumfahrttechnik (DE-588)4177061-4 gnd Raumfahrt (DE-588)4048574-2 gnd Luftfahrttechnik (DE-588)4168244-0 gnd
topic_facet	Aerodynamics Airplanes Design and construction Space flight Flugzeugbau Flugmechanik Aerodynamik Raumfahrttechnik Raumfahrt Luftfahrttechnik Einführung
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