Fundamentals of aerodynamics:
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| Main Author: | |
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| Format: | Book |
| Language: | English |
| Published: |
New York, NY [u.a.]
McGraw-Hill Higher Education
2007
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| Edition: | 4. ed. |
| Series: | McGraw-Hill series in aeronautical and aerospace engineering
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| Subjects: | |
| Online Access: | Table of contents only Publisher description Inhaltsverzeichnis |
| Item Description: | Includes bibliographical references (p. 981-985) and index |
| Physical Description: | XXIV, 1008 S. Ill., graph. Darst. 24 cm |
| ISBN: | 9780072950465 0072950463 |
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| 245 | 1 | 0 | |a Fundamentals of aerodynamics |c John D. Anderson |
| 250 | |a 4. ed. | ||
| 264 | 1 | |a New York, NY [u.a.] |b McGraw-Hill Higher Education |c 2007 | |
| 300 | |a XXIV, 1008 S. |b Ill., graph. Darst. |c 24 cm | ||
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| 500 | |a Includes bibliographical references (p. 981-985) and index | ||
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| 650 | 4 | |a Aérodynamique | |
| 650 | 4 | |a Aerodynamics | |
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| adam_text | FUNDAMENTALS OF AERODYNAMICS FOURTH EDITION JOHN D. ANDERSON, JR.
CURATOR OF AERODYNAMICS NATIONAL AIR AND SPACE MUSEUM SMITHSONIAN
INSTITUTION AND PROFESSOR EMERITUS UNIVERSITY OF MARYLAND ME GRAW HILL
HIGHER EDUCATION 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 PREFACE TO THE FIRST EDITION
XIX PREFACE TO THE FOURTH EDITION XXIII PART J. FUNDAMENTAL PRINCIPLES 1
CHAPTER 1 AERODYNAMICS: SOME INTRODUCTORY THOUGHTS 3 1.1 IMPORTANCE OF
AERODYNAMICS: HISTORICAL EXAMPLES 5 1.2 AERODYNAMICS: CLASSIFICATION AND
PRACTICAL OBJECTIVES 11 1.3 ROAD MAP FOR THIS CHAPTER 14 1.4 SOME
FUNDAMENTAL AERODYNAMIC VARIABLES 15 1.4.1 UNITS 18 1.5 AERODYNAMIC
FORCES AND MOMENTS 19 1.6 CENTER OF PRESSURE 32 1.7 DIMENSIONAL
ANALYSIS: THE BUCKINGHAM PI THEOREM 34 1.8 FLOW SIMILARITY 40 1.9 FLUID
STATICS: BUOYANCY FORCE 51 1.10 TYPES OF FLOW 57 1.10.1 CONTINUUM VERSUS
FREE MOLECULE FLOW 58 1.10.2 INVISCID VERSUS VISCOUS FLOW 58 1.10.3
INCOMPRESSIBLE VERSUS COMPRESSIBLE FLOWS 60 1.10.4 MACH NUMBER REGIMES
60 1.11 VISCOUS FLOW: INTRODUCTION TO BOUNDARY LAYERS 64 1.12 APPLIED
AERODYNAMICS: THE AERODYNAMIC COEFFICIENTS*THEIR MAGNITUDES AND
VARIATIONS 71 1.13 HISTORICAL NOTE: THE ILLUSIVE CENTER OF PRESSURE 83
1.14 HISTORICAL NOTE: AERODYNAMIC COEFFICIENTS 87 1.15 SUMMARY 91 1.16
PROBLEMS 92 CHAPTER 2 AERODYNAMICS: SOME FUNDAMENTAL PRINCIPLES AND
EQUATIONS 95 2.1 INTRODUCTION AND ROAD MAP 96 2.2 REVIEW OF VECTOR
RELATIONS 97 2.2.1 SOME VECTOR ALGEBRA 98 2.2.2 TYPICAL ORTHOGONAL
COORDINATE SYSTEMS 99 2.2.3 SCALAR AND VECTOR FIELDS 102 2.2.4 SCALAR
AND VECTOR PRODUCTS 102 2.2.5 GRADIENT OF A SCALAR FIELD 103 2.2.6
DIVERGENCE OF A VECTOR FIELD 105 2.2.7 CURL OF A VECTOR FIELD 106 2.2.8
LINE INTEGRALS 106 2.2.9 SURFACE INTEGRALS 107 2.2.10 VOLUME INTEGRALS
108 2.2.11 RELATIONS BETWEEN LINE, SURFACE, AND VOLUME INTEGRALS 109
2.2.12 SUMMARY 109 2.3 MODELS OF THE FLUID: CONTROL VOLUMES AND FLUID
ELEMENTS 109 2.3.1 FINITE CONTROL VOLUME APPROACH 110 2.3.2
INFINITESIMAL FLUID ELEMENT APPROACH 111 2.3.3 MOLECULAR APPROACH 111
XII CONTENTS 2.4 2.5 2.6 2.7 2.8 2.9 2.3.4 PHYSICAL MEANING OF THE
DIVERGENCE OF VELOCITY 112 2.3.5 SPECIFICATION OF THE FLOW FIELD 113
CONTINUITY EQUATION 117 MOMENTUM EQUATION 122 AN APPLICATION OF THE
MOMENTUM EQUATION: DRAG OF A TWO-DIMENSIONAL BODY 127 2.6.1 COMMENT 136
ENERGY EQUATION 136 INTERIM SUMMARY 141 SUBSTANTIAL DERIVATIVE 142 2.10
FUNDAMENTAL EQUATIONS IN TERMS OF THE SUBSTANTIAL DERIVATIVE 145 2.11
PATHLINES, STREAMLINES, AND STREAKLINES OF A FLOW 147 2.12 ANGULAR
VELOCITY, VORTICITY, AND STRAIN 152 2.13 CIRCULATION 162 2.14 STREAM
FUNCTION 165 2.15 VELOCITY POTENTIAL 169 2.16 RELATIONSHIP BETWEEN THE
STREAM FUNCTION AND VELOCITY POTENTIAL 171 2.17 HOW DO WE SOLVE THE
EQUATIONS? 172 2.17.1 THEORETICAL (ANALYTICAL) SOLUTIONS 172 2.17.2
NUMERICAL SOLUTIONS * COMPUTATIONAL FLUID DYNAMICS (CFD) 174 2.17.3 THE
BIGGER PICTURE 181 2.18 SUMMARY 181 2.19 PROBLEMS 185 PART TNVJSCIRT,
INCOMPRESSIBLE FLOW 187 CHAPTER 3 FUNDAMENTALS OF INVISCID,
INCOMPRESSIBLE FLOW 189 3.1 INTRODUCTION AND ROAD MAP 3.2 BERNOULLI S
EQUATION 193 190 3.3 INCOMPRESSIBLE FLOW IN A DUCT: THE VENTURI AND
LOW-SPEED WIND TUNNEL 197 3.4 PITOT TUBE: MEASUREMENT OF AIRSPEED 210
3.5 PRESSURE COEFFICIENT 219 3.6 CONDITION ON VELOCITY FOR
INCOMPRESSIBLE FLOW 221 3.7 GOVERNING EQUATION FOR IRROTATIONAL,
INCOMPRESSIBLE FLOW: LAPLACE S EQUATION 222 3. 7. 1 INFINITY BOUNDARY
CONDITIONS 225 3.7.2 WALL BOUNDARY CONDITIONS 225 3.8 INTERIM SUMMARY
226 3.9 UNIFORM FLOW: OUR FIRST ELEMENTARY FLOW 227 3.10 SOURCE FLOW:
OUR SECOND ELEMENTARY FLOW 229 3.11 COMBINATION OF A UNIFORM FLOW WITH A
SOURCE AND SINK 233 3.12 DOUBLET FLOW: OUR THIRD ELEMENTARY FLOW 237
3.13 NONLIFTING FLOW OVER A CIRCULAR CYLINDER 239 3.14 VORTEX FLOW: OUR
FOURTH ELEMENTARY FLOW 245 3.15 LIFTING FLOW OVER A CYLINDER 249 3.16
THE KUTTA-JOUKOWSKI THEOREM AND THE GENERATION OF LIFT 262 3.17
NONLIFTING FLOWS OVER ARBITRARY BODIES: THE NUMERICAL SOURCE PANEL
METHOD 264 3.18 APPLIED AERODYNAMICS: THE FLOW OVER A CIRCULAR
CYLINDER*THE REAL CASE 274 3.19 HISTORICAL NOTE: BERNOULLI AND EULER*THE
ORIGINS OF THEORETICAL FLUID DYNAMICS 282 3.20 HISTORICAL NOTE:
D ALEMBERT AND HIS PARADOX 287 3.21 SUMMARY 288 3.22 PROBLEMS 291
CONTENTS XIII CHAPTER 4 INCOMPRESSIBLE FLOW OVER AIRFOILS 295 4.1
INTRODUCTION 297 4.2 AIRFOIL NOMENCLATURE 300 4.3 AIRFOIL
CHARACTERISTICS 302 4.4 PHILOSOPHY OF THEORETICAL SOLUTIONS FOR
LOW-SPEED FLOW OVER AIRFOILS: THE VORTEX SHEET 307 4.5 THE KUTTA
CONDITION 312 4.5.1 WITHOUT FRICTION COULD WE HAVE LIFT? 316 4.6
KELVIN S CIRCULATION THEOREM AND THE STARTING VORTEX 316 4.7 CLASSICAL
THIN AIRFOIL THEORY: THE SYMMETRIC AIRFOIL 319 4.8 THE CAMBERED AIRFOIL
329 4.9 THE AERODYNAMIC CENTER: ADDITIONAL CONSIDERATIONS 338 4.10
LIFTING FLOWS OVER ARBITRARY BODIES: THE VORTEX PANEL NUMERICAL METHOD
342 4.11 MODERN LOW-SPEED AIRFOILS 348 4.12 VISCOUS FLOW: AIRFOIL DRAG
352 4.12.1 ESTIMATING SKIN-FRICTION DRAG: LAMINAR FLOW 353 4.12.2
ESTIMATING SKIN-FRICTION DRAG: TURBULENT FLOW 355 4.12.3 TRANSITION 357
4.12.4 FLOW SEPARATION 362 4.12.5 COMMENT 367 4.13 APPLIED AERODYNAMICS:
THE FLOW OVER AN AIRFOIL*THE REAL CASE 368 4.14 HISTORICAL NOTE: EARLY
AIRPLANE DESIGN AND THE ROLE OF AIRFOIL THICKNESS 379 4.15 HISTORICAL
NOTE: KUTTA, JOUKOWSKI, AND THE CIRCULATION THEORY OF LIFT 384 4.16
SUMMARY 386 4.17 PROBLEMS 388 CHAPTER 5 INCOMPRESSIBLE FLOW OVER FINITE
WINGS 391 5.1 INTRODUCTION: DOWNWASH AND INDUCED DRAG 395 5.2 THE VORTEX
FILAMENT, THE BIOT-SAVART LAW, AND HELMHOLTZ S THEOREMS 400 5.3
PRANDTL S CLASSICAL LIFTING-LINE THEORY 404 5.3.1 ELLIPTICAL LIFT
DISTRIBUTION 410 5.3.2 GENERAL LIFT DISTRIBUTION 415 5.3.3 EFFECT OF
ASPECT RATIO 418 5.3.4 PHYSICAL SIGNIFICANCE 424 5.4 A NUMERICAL
NONLINEAR LIFTING-LINE METHOD 433 5.5 THE LIFTING-SURFACE THEORY AND THE
VORTEX LATTICE NUMERICAL METHOD 437 5.6 APPLIED AERODYNAMICS: THE DELTA
WING 444 5.7 HISTORICAL NOTE: LANCHESTER AND PRANDTL*THE EARLY
DEVELOPMENT OF FINITE-WING THEORY 456 5.8 HISTORICAL NOTE: PRANDTL*THE
MAN 460 5.9 SUMMARY 463 5.10 PROBLEMS 464 CHAPTER 6 THREE-DIMENSIONAL
INCOMPRESSIBLE FLOW 467 6.1 INTRODUCTION 467 6.2 THREE-DIMENSIONAL
SOURCE 468 6.3 THREE-DIMENSIONAL DOUBLET 470 6.4 FLOW OVER A SPHERE 472
6.4.1 COMMENT ON THE THREE-DIMENSIONAL RELIEVING EFFECT 474 6.5 GENERAL
THREE-DIMENSIONAL FLOWS: PANEL TECHNIQUES 475 6.6 APPLIED AERODYNAMICS:
THE FLOW OVER A SPHERE*THE REAL CASE 477 6.7 SUMMARY 480 6.8 PROBLEMS
481 XIV CONTENTS PART MJ TNVISCID, COMPRESSIBLE FLOW 483 CHAPTER 7
COMPRESSIBLE FLOW: SOME PRELIMINARY ASPECTS 485 7.1 INTRODUCTION 486 7.2
A BRIEF REVIEW OF THERMODYNAMICS 488 7.2.1 PERFECT GAS 488 7.2.2
INTERNAL ENERGY AND ENTHALPY 488 7.2.3 FIRST LAW OF THERMODYNAMICS 492
7.2.4 ENTROPY AND THE SECOND LAW OF THERMODYNAMICS 493 7.2.5 ISENTROPIC
RELATIONS 495 7.3 DEFINITION OF COMPRESSIBILITY 497 7.4 GOVERNING
EQUATIONS FOR INVISCID, COMPRESSIBLE FLOW 499 7.5 DEFINITION OF TOTAL
(STAGNATION) CONDITIONS 501 7.6 SOME ASPECTS OF SUPERSONIC FLOW: SHOCK
WAVES 507 7.7 SUMMARY 510 7.8 PROBLEMS 513 CHAPTER 8 NORMAL SHOCK WAVES
AND RELATED TOPICS 515 8.1 INTRODUCTION 516 8.2 TH E BASIC NORMAL SHOCK
EQUATIONS 517 8.3 SPEED OF SOUND 521 8.4 SPECIAL FORMS OF THE ENERGY
EQUATION 527 8.5 WHEN IS A FLOW COMPRESSIBLE? 534 8.6 CALCULATION OF
NORMAL SHOCK-WAVE PROPERTIES 537 8.7 MEASUREMENT OF VELOCITY IN A
COMPRESSIBLE FLOW 548 8.7.7 SUBSONIC COMPRESSIBLE FLOW 548 8.7.2
SUPERSONIC FLOW 549 8.8 SUMMARY 553 8.9 PROBLEMS 556 CHAPTER 9 OBLIQUE
SHOCK AND EXPANSION WAVES 559 9.1 INTRODUCTION 560 9.2 OBLIQUE SHOCK
RELATIONS 566 9.3 SUPERSONIC FLOW OVER WEDGES AND CONES 580 9.4 SHOCK
INTERACTIONS AND REFLECTIONS 583 9.5 DETACHED SHOCK WAVE IN FRONT OF A
BLUNT BODY 589 9.6 PRANDTL-MEYER EXPANSION WAVES 591 9.7 SHOCK-EXPANSION
THEORY: APPLICATIONS TO SUPERSONIC AIRFOILS 602 9.8 A COMMENT ON LIFT
AND DRAG COEFFICIENTS 606 9.9 VISCOUS FLOW: SHOCK-WAVE/ BOUNDARY-LAYER
INTERACTION 606 9.10 HISTORICAL NOTE: ERNST MACH*A BIOGRAPHICAL SKETCH
609 9.11 SUMMARY 611 9.12 PROBLEMS 612 CHAPTER 10 COMPRESSIBLE FLOW
THROUGH NOZZLES, DIFFUSERS, AND WIND TUNNELS 617 10.1 INTRODUCTION 618
10.2 GOVERNING EQUATIONS FOR QUASI-ONE-DIMENSIONAL FLOW 620 10.3 NOZZLE
FLOWS 629 10.3.1 MORE ON MASS FLOW 643 10.4 DIFFUSERS 644 10.5
SUPERSONIC WIND TUNNELS 646 10.6 VISCOUS FLOW: SHOCK-WAVE/
BOUNDARY-LAYER INTERACTION INSIDE NOZZLES 652 10.7 SUMMARY 654 10.8
PROBLEMS 655 CONTENTS CHAPTER 11 SUBSONIC COMPRESSIBLE FLOW OVER
AIRFOILS: LINEAR THEORY 657 11.1 INTRODUCTION 658 11.2 THE VELOCITY
POTENTIAL EQUATION 660 11.3 THE LINEARIZED VELOCITY POTENTIAL EQUATION
663 11.4 PRANDTL-GLAUERT COMPRESSIBILITY CORRECTION 668 11.5 IMPROVED
COMPRESSIBILITY CORRECTIONS 673 11.6 CRITICAL MACH NUMBER 674 11.6.1 A
COMMENT ON THE LOCATION OF MINIMUM PRESSURE (MAXIMUM VELOCITY) 683 11.7
DRAG-DIVERGENCE MACH NUMBER: THE SOUND BARRIER 683 11.8 THE AREA RULE
691 11.9 THE SUPERCRITICAL AIRFOIL 693 11.10 CFD APPLICATIONS: TRANSONIC
AIRFOILS AND WINGS 695 11.11 HISTORICAL NOTE: HIGH-SPEED AIRFOILS*EARLY
RESEARCH AND DEVELOPMENT 700 11.12 HISTORICAL NOTE: RICHARD T. WHITCOMB*
ARCHITECT OF THE AREA RULE AND THE SUPERCRITICAL WING 704 11.13 SUMMARY
706 11.14 PROBLEMS 707 CHAPTER 12 LINEARIZED SUPERSONIC FLOW 709 12.1
INTRODUCTION 710 12.2 DERIVATION OF THE LINEARIZED SUPERSONIC PRESSURE
COEFFICIENT FORMULA 710 12.3 APPLICATION TO SUPERSONIC AIRFOILS 714 12.4
VISCOUS FLOW: SUPERSONIC AIRFOIL DRAG 720 12.5 SUMMARY 723 12.6 PROBLEMS
724 CHAPTER 13 INTRODUCTION TO NUMERICAL TECHNIQUES FOR NONLINEAR
SUPERSONIC FLOW 725 13.1 INTRODUCTION: PHILOSOPHY OF COMPUTATIONAL FLUID
DYNAMICS 726 13.2 ELEMENTS OF THE METHOD OF CHARACTERISTICS 728 13.2.1
INTERNAL POINTS 734 13.2.2 WALL POINTS 735 13.3 SUPERSONIC NOZZLE DESIGN
736 13.4 ELEMENTS OF FINITE-DIFFERENCE METHODS 739 13.4.1 PREDICTOR STEP
745 13.4.2 CORRECTOR STEP 745 13.5 THE TIME-DEPENDENT TECHNIQUE:
APPLICATION TO SUPERSONIC BLUNT BODIES 746 13.5.1 PREDICTOR STEP 750
13.5.2 CORRECTOR STEP 750 13.6 SUMMARY 754 13.7 PROBLEM 754 CHAPTER 14
ELEMENTS OF HYPERSONIC FLOW 757 14.1 INTRODUCTION 758 14.2 QUALITATIVE
ASPECTS OF HYPERSONIC FLOW 759 14.3 NEWTONIAN THEORY 763 14.4 THE LIFT
AND DRAG OF WINGS AT HYPERSONIC SPEEDS: NEWTONIAN RESULTS FOR A FLAT
PLATE AT ANGLE OF ATTACK 767 14.4.1 ACCURACY CONSIDERATIONS 774 14.5
HYPERSONIC SHOCK-WAVE RELATIONS AND ANOTHER LOOK AT NEWTONIAN THEORY 778
14.6 MACH NUMBER INDEPENDENCE 782 14.7 HYPERSONICS AND COMPUTATIONAL
FLUID DYNAMICS 784 14.8 SUMMARY 787 14.9 PROBLEMS 787 XVI CONTENTS PART
*T VISCOUS FLOW 789 CHAPTER 15 INTRODUCTION TO THE FUNDAMENTAL
PRINCIPLES AND EQUATIONS OF VISCOUS FLOW 791 15.1 INTRODUCTION 792 15.2
QUALITATIVE ASPECTS OF VISCOUS FLOW 793 15.3 VISCOSITY AND THERMAL
CONDUCTION 801 15.4 THE NAVIER-STOKES EQUATIONS 806 15.5 THE VISCOUS
FLOW ENERGY EQUATION 810 15.6 SIMILARITY PARAMETERS 814 15.7 SOLUTIONS
OF VISCOUS FLOWS: A PRELIMINARY DISCUSSION 818 15.8 SUMMARY 821 15.9
PROBLEMS 823 CHAPTER 16 SOME SPECIAL CASES; COUETTE AND POISEUILLE FLOWS
825 16.1 INTRODUCTION 825 16.2 COUETTE FLOW: GENERAL DISCUSSION 826 16.3
INCOMPRESSIBLE (CONSTANT PROPERTY) COUETTE FLOW 830 16.3.1 NEGLIGIBLE
VISCOUS DISSIPATION 836 16.3.2 EQUAL WALL TEMPERATURES 837 16.3.3
ADIABATIC WALL CONDITIONS (ADIABATIC WALL TEMPERATURE) 839 16.3.4
RECOVERY FACTOR 842 16.3.5 REYNOLDS ANALOGY 843 16.3.6 INTERIM SUMMARY
844 16.4 COMPRESSIBLE COUETTE FLOW 846 16.4.1 SHOOTING METHOD 848 16.4.2
TIME-DEPENDENT FINITE-DIFFERENCE METHOD 850 16.4.3 RESULTS FOR
COMPRESSIBLE COUETTE FLOW 854 16.4.4 SOME ANALYTICAL CONSIDERATIONS 856
16.5 TWO-DIMENSIONAL POISEUILLE FLOW 861 16.6 SUMMARY 865 16.6.1 COUETTE
FLOW 865 16.6.2 POISEUILLE FLOW 865 CHAPTER 17 INTRODUCTION TO BOUNDARY
LAYERS 867 17.1 INTRODUCTION 868 17.2 BOUNDARY-LAYER PROPERTIES 870 17.3
THE BOUNDARY-LAYER EQUATIONS 876 17.4 HOW DO WE SOLVE THE BOUNDARY-LAYER
EQUATIONS? 879 17.5 SUMMARY 881 CHAPTER 18 LAMINAR BOUNDARY LAYERS 883
18.1 INTRODUCTION 883 18.2 INCOMPRESSIBLE FLOW OVER A FLAT PLATE: THE
BLASIUS SOLUTION 884 18.3 COMPRESSIBLE FLOW OVER A FLAT PLATE 891 18.3.1
A COMMENT ON DRAG VARIATION WITH VELOCITY 902 18.4 THE REFERENCE
TEMPERATURE METHOD 903 18.4.1 RECENT ADVANCES: THE MEADOR-SMART
REFERENCE TEMPERATURE METHOD 906 18.5 STAGNATIO N POINT AERODYNAMIC
HEATING 907 18.6 BOUNDARY LAYERS OVER ARBITRARY BODIES:
FINITE-DIFFERENCE SOLUTION 913 18.6.1 FINITE-DIFFERENCE METHOD 914 18.7
SUMMARY 919 18.8 PROBLEMS 920 CHAPTER 19 TURBULENT BOUNDARY LAYERS 921
19.1 INTRODUCTION 922 19.2 RESULTS FOR TURBULENT BOUNDARY LAYERS ON A
FLAT PLATE 922 CONTENTS XVII 19.2.1 REFERENCE TEMPERATURE METHOD FOR
TURBULENT FLOW 924 19.2.2 THE MEADOR-SMART REFERENCE TEMPERATURE METHOD
FOR TURBULENT FLOW 926 19.2.3 PREDICTION OF AIRFOIL DRAG 927 19.3
TURBULENCE MODELING 927 19.3.1 THE BALDWIN-LOMAX MODEL 928 19.4 FINAL
COMMENTS 930 19.5 SUMMARY 931 19.6 PROBLEMS 932 CHAPTER 20 NAVIER-STOKES
SOLUTIONS: SOME EXAMPLES 933 20.1 INTRODUCTION 934 20.2 THE APPROACH 934
20.3 EXAMPLES OF SOME SOLUTIONS 935 20.3.1 FLOW OVER A REARWARD-FACING
STEP 935 20.3.2 FLOW OVER AN AIRFOIL 935 20.3.3 FLOW OVER A COMPLETE
AIRPLANE 938 20.3.4 SHOCK-WAVE/BOUNDARY-LAYER INTERACTION 939 20.3.5
FLOW OVER AN AIRFOIL WITH A PROTUBERANCE 940 20.4 THE ISSUE OF ACCURACY
FOR THE PREDICTION OF SKIN FRICTION DRAG 942 20.5 SUMMARY 947 APPENDIX A
ISENTROPIC FLOW PROPERTIES 949 APPENDIX B NORMAL SHOCK PROPERTIES 955
APPENDIX C PRANDTL-MEYER FUNCTION AND MACH ANGLE 959 APPENDIX D STANDARD
ATMOSPHERE, SI UNITS 963 APPENDIX E STANDARD ATMOSPHERE, ENGLISH
ENGINEERING UNITS 973 BIBLIOGRAPHY 981 INDEX 987
|
| adam_txt |
FUNDAMENTALS OF AERODYNAMICS FOURTH EDITION JOHN D. ANDERSON, JR.
CURATOR OF AERODYNAMICS NATIONAL AIR AND SPACE MUSEUM SMITHSONIAN
INSTITUTION AND PROFESSOR EMERITUS UNIVERSITY OF MARYLAND ME GRAW HILL
HIGHER EDUCATION 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 PREFACE TO THE FIRST EDITION
XIX PREFACE TO THE FOURTH EDITION XXIII PART J. FUNDAMENTAL PRINCIPLES 1
CHAPTER 1 AERODYNAMICS: SOME INTRODUCTORY THOUGHTS 3 1.1 IMPORTANCE OF
AERODYNAMICS: HISTORICAL EXAMPLES 5 1.2 AERODYNAMICS: CLASSIFICATION AND
PRACTICAL OBJECTIVES 11 1.3 ROAD MAP FOR THIS CHAPTER 14 1.4 SOME
FUNDAMENTAL AERODYNAMIC VARIABLES 15 1.4.1 UNITS 18 1.5 AERODYNAMIC
FORCES AND MOMENTS 19 1.6 CENTER OF PRESSURE 32 1.7 DIMENSIONAL
ANALYSIS: THE BUCKINGHAM PI THEOREM 34 1.8 FLOW SIMILARITY 40 1.9 FLUID
STATICS: BUOYANCY FORCE 51 1.10 TYPES OF FLOW 57 1.10.1 CONTINUUM VERSUS
FREE MOLECULE FLOW 58 1.10.2 INVISCID VERSUS VISCOUS FLOW 58 1.10.3
INCOMPRESSIBLE VERSUS COMPRESSIBLE FLOWS 60 1.10.4 MACH NUMBER REGIMES
60 1.11 VISCOUS FLOW: INTRODUCTION TO BOUNDARY LAYERS 64 1.12 APPLIED
AERODYNAMICS: THE AERODYNAMIC COEFFICIENTS*THEIR MAGNITUDES AND
VARIATIONS 71 1.13 HISTORICAL NOTE: THE ILLUSIVE CENTER OF PRESSURE 83
1.14 HISTORICAL NOTE: AERODYNAMIC COEFFICIENTS 87 1.15 SUMMARY 91 1.16
PROBLEMS 92 CHAPTER 2 AERODYNAMICS: SOME FUNDAMENTAL PRINCIPLES AND
EQUATIONS 95 2.1 INTRODUCTION AND ROAD MAP 96 2.2 REVIEW OF VECTOR
RELATIONS 97 2.2.1 SOME VECTOR ALGEBRA 98 2.2.2 TYPICAL ORTHOGONAL
COORDINATE SYSTEMS 99 2.2.3 SCALAR AND VECTOR FIELDS 102 2.2.4 SCALAR
AND VECTOR PRODUCTS 102 2.2.5 GRADIENT OF A SCALAR FIELD 103 2.2.6
DIVERGENCE OF A VECTOR FIELD 105 2.2.7 CURL OF A VECTOR FIELD 106 2.2.8
LINE INTEGRALS 106 2.2.9 SURFACE INTEGRALS 107 2.2.10 VOLUME INTEGRALS
108 2.2.11 RELATIONS BETWEEN LINE, SURFACE, AND VOLUME INTEGRALS 109
2.2.12 SUMMARY 109 2.3 MODELS OF THE FLUID: CONTROL VOLUMES AND FLUID
ELEMENTS 109 2.3.1 FINITE CONTROL VOLUME APPROACH 110 2.3.2
INFINITESIMAL FLUID ELEMENT APPROACH 111 2.3.3 MOLECULAR APPROACH 111
XII CONTENTS 2.4 2.5 2.6 2.7 2.8 2.9 2.3.4 PHYSICAL MEANING OF THE
DIVERGENCE OF VELOCITY 112 2.3.5 SPECIFICATION OF THE FLOW FIELD 113
CONTINUITY EQUATION 117 MOMENTUM EQUATION 122 AN APPLICATION OF THE
MOMENTUM EQUATION: DRAG OF A TWO-DIMENSIONAL BODY 127 2.6.1 COMMENT 136
ENERGY EQUATION 136 INTERIM SUMMARY 141 SUBSTANTIAL DERIVATIVE 142 2.10
FUNDAMENTAL EQUATIONS IN TERMS OF THE SUBSTANTIAL DERIVATIVE 145 2.11
PATHLINES, STREAMLINES, AND STREAKLINES OF A FLOW 147 2.12 ANGULAR
VELOCITY, VORTICITY, AND STRAIN 152 2.13 CIRCULATION 162 2.14 STREAM
FUNCTION 165 2.15 VELOCITY POTENTIAL 169 2.16 RELATIONSHIP BETWEEN THE
STREAM FUNCTION AND VELOCITY POTENTIAL 171 2.17 HOW DO WE SOLVE THE
EQUATIONS? 172 2.17.1 THEORETICAL (ANALYTICAL) SOLUTIONS 172 2.17.2
NUMERICAL SOLUTIONS * COMPUTATIONAL FLUID DYNAMICS (CFD) 174 2.17.3 THE
BIGGER PICTURE 181 2.18 SUMMARY 181 2.19 PROBLEMS 185 PART TNVJSCIRT,
INCOMPRESSIBLE FLOW 187 CHAPTER 3 FUNDAMENTALS OF INVISCID,
INCOMPRESSIBLE FLOW 189 3.1 INTRODUCTION AND ROAD MAP 3.2 BERNOULLI'S
EQUATION 193 190 3.3 INCOMPRESSIBLE FLOW IN A DUCT: THE VENTURI AND
LOW-SPEED WIND TUNNEL 197 3.4 PITOT TUBE: MEASUREMENT OF AIRSPEED 210
3.5 PRESSURE COEFFICIENT 219 3.6 CONDITION ON VELOCITY FOR
INCOMPRESSIBLE FLOW 221 3.7 GOVERNING EQUATION FOR IRROTATIONAL,
INCOMPRESSIBLE FLOW: LAPLACE'S EQUATION 222 3. 7. 1 INFINITY BOUNDARY
CONDITIONS 225 3.7.2 WALL BOUNDARY CONDITIONS 225 3.8 INTERIM SUMMARY
226 3.9 UNIFORM FLOW: OUR FIRST ELEMENTARY FLOW 227 3.10 SOURCE FLOW:
OUR SECOND ELEMENTARY FLOW 229 3.11 COMBINATION OF A UNIFORM FLOW WITH A
SOURCE AND SINK 233 3.12 DOUBLET FLOW: OUR THIRD ELEMENTARY FLOW 237
3.13 NONLIFTING FLOW OVER A CIRCULAR CYLINDER 239 3.14 VORTEX FLOW: OUR
FOURTH ELEMENTARY FLOW 245 3.15 LIFTING FLOW OVER A CYLINDER 249 3.16
THE KUTTA-JOUKOWSKI THEOREM AND THE GENERATION OF LIFT 262 3.17
NONLIFTING FLOWS OVER ARBITRARY BODIES: THE NUMERICAL SOURCE PANEL
METHOD 264 3.18 APPLIED AERODYNAMICS: THE FLOW OVER A CIRCULAR
CYLINDER*THE REAL CASE 274 3.19 HISTORICAL NOTE: BERNOULLI AND EULER*THE
ORIGINS OF THEORETICAL FLUID DYNAMICS 282 3.20 HISTORICAL NOTE:
D'ALEMBERT AND HIS PARADOX 287 3.21 SUMMARY 288 3.22 PROBLEMS 291
CONTENTS XIII CHAPTER 4 INCOMPRESSIBLE FLOW OVER AIRFOILS 295 4.1
INTRODUCTION 297 4.2 AIRFOIL NOMENCLATURE 300 4.3 AIRFOIL
CHARACTERISTICS 302 4.4 PHILOSOPHY OF THEORETICAL SOLUTIONS FOR
LOW-SPEED FLOW OVER AIRFOILS: THE VORTEX SHEET 307 4.5 THE KUTTA
CONDITION 312 4.5.1 WITHOUT FRICTION COULD WE HAVE LIFT? 316 4.6
KELVIN'S CIRCULATION THEOREM AND THE STARTING VORTEX 316 4.7 CLASSICAL
THIN AIRFOIL THEORY: THE SYMMETRIC AIRFOIL 319 4.8 THE CAMBERED AIRFOIL
329 4.9 THE AERODYNAMIC CENTER: ADDITIONAL CONSIDERATIONS 338 4.10
LIFTING FLOWS OVER ARBITRARY BODIES: THE VORTEX PANEL NUMERICAL METHOD
342 4.11 MODERN LOW-SPEED AIRFOILS 348 4.12 VISCOUS FLOW: AIRFOIL DRAG
352 4.12.1 ESTIMATING SKIN-FRICTION DRAG: LAMINAR FLOW 353 4.12.2
ESTIMATING SKIN-FRICTION DRAG: TURBULENT FLOW 355 4.12.3 TRANSITION 357
4.12.4 FLOW SEPARATION 362 4.12.5 COMMENT 367 4.13 APPLIED AERODYNAMICS:
THE FLOW OVER AN AIRFOIL*THE REAL CASE 368 4.14 HISTORICAL NOTE: EARLY
AIRPLANE DESIGN AND THE ROLE OF AIRFOIL THICKNESS 379 4.15 HISTORICAL
NOTE: KUTTA, JOUKOWSKI, AND THE CIRCULATION THEORY OF LIFT 384 4.16
SUMMARY 386 4.17 PROBLEMS 388 CHAPTER 5 INCOMPRESSIBLE FLOW OVER FINITE
WINGS 391 5.1 INTRODUCTION: DOWNWASH AND INDUCED DRAG 395 5.2 THE VORTEX
FILAMENT, THE BIOT-SAVART LAW, AND HELMHOLTZ'S THEOREMS 400 5.3
PRANDTL'S CLASSICAL LIFTING-LINE THEORY 404 5.3.1 ELLIPTICAL LIFT
DISTRIBUTION 410 5.3.2 GENERAL LIFT DISTRIBUTION 415 5.3.3 EFFECT OF
ASPECT RATIO 418 5.3.4 PHYSICAL SIGNIFICANCE 424 5.4 A NUMERICAL
NONLINEAR LIFTING-LINE METHOD 433 5.5 THE LIFTING-SURFACE THEORY AND THE
VORTEX LATTICE NUMERICAL METHOD 437 5.6 APPLIED AERODYNAMICS: THE DELTA
WING 444 5.7 HISTORICAL NOTE: LANCHESTER AND PRANDTL*THE EARLY
DEVELOPMENT OF FINITE-WING THEORY 456 5.8 HISTORICAL NOTE: PRANDTL*THE
MAN 460 5.9 SUMMARY 463 5.10 PROBLEMS 464 CHAPTER 6 THREE-DIMENSIONAL
INCOMPRESSIBLE FLOW 467 6.1 INTRODUCTION 467 6.2 THREE-DIMENSIONAL
SOURCE 468 6.3 THREE-DIMENSIONAL DOUBLET 470 6.4 FLOW OVER A SPHERE 472
6.4.1 COMMENT ON THE THREE-DIMENSIONAL RELIEVING EFFECT 474 6.5 GENERAL
THREE-DIMENSIONAL FLOWS: PANEL TECHNIQUES 475 6.6 APPLIED AERODYNAMICS:
THE FLOW OVER A SPHERE*THE REAL CASE 477 6.7 SUMMARY 480 6.8 PROBLEMS
481 XIV CONTENTS PART MJ TNVISCID, COMPRESSIBLE FLOW 483 CHAPTER 7
COMPRESSIBLE FLOW: SOME PRELIMINARY ASPECTS 485 7.1 INTRODUCTION 486 7.2
A BRIEF REVIEW OF THERMODYNAMICS 488 7.2.1 PERFECT GAS 488 7.2.2
INTERNAL ENERGY AND ENTHALPY 488 7.2.3 FIRST LAW OF THERMODYNAMICS 492
7.2.4 ENTROPY AND THE SECOND LAW OF THERMODYNAMICS 493 7.2.5 ISENTROPIC
RELATIONS 495 7.3 DEFINITION OF COMPRESSIBILITY 497 7.4 GOVERNING
EQUATIONS FOR INVISCID, COMPRESSIBLE FLOW 499 7.5 DEFINITION OF TOTAL
(STAGNATION) CONDITIONS 501 7.6 SOME ASPECTS OF SUPERSONIC FLOW: SHOCK
WAVES 507 7.7 SUMMARY 510 7.8 PROBLEMS 513 CHAPTER 8 NORMAL SHOCK WAVES
AND RELATED TOPICS 515 8.1 INTRODUCTION 516 8.2 TH E BASIC NORMAL SHOCK
EQUATIONS 517 8.3 SPEED OF SOUND 521 8.4 SPECIAL FORMS OF THE ENERGY
EQUATION 527 8.5 WHEN IS A FLOW COMPRESSIBLE? 534 8.6 CALCULATION OF
NORMAL SHOCK-WAVE PROPERTIES 537 8.7 MEASUREMENT OF VELOCITY IN A
COMPRESSIBLE FLOW 548 8.7.7 SUBSONIC COMPRESSIBLE FLOW 548 8.7.2
SUPERSONIC FLOW 549 8.8 SUMMARY 553 8.9 PROBLEMS 556 CHAPTER 9 OBLIQUE
SHOCK AND EXPANSION WAVES 559 9.1 INTRODUCTION 560 9.2 OBLIQUE SHOCK
RELATIONS 566 9.3 SUPERSONIC FLOW OVER WEDGES AND CONES 580 9.4 SHOCK
INTERACTIONS AND REFLECTIONS 583 9.5 DETACHED SHOCK WAVE IN FRONT OF A
BLUNT BODY 589 9.6 PRANDTL-MEYER EXPANSION WAVES 591 9.7 SHOCK-EXPANSION
THEORY: APPLICATIONS TO SUPERSONIC AIRFOILS 602 9.8 A COMMENT ON LIFT
AND DRAG COEFFICIENTS 606 9.9 VISCOUS FLOW: SHOCK-WAVE/ BOUNDARY-LAYER
INTERACTION 606 9.10 HISTORICAL NOTE: ERNST MACH*A BIOGRAPHICAL SKETCH
609 9.11 SUMMARY 611 9.12 PROBLEMS 612 CHAPTER 10 COMPRESSIBLE FLOW
THROUGH NOZZLES, DIFFUSERS, AND WIND TUNNELS 617 10.1 INTRODUCTION 618
10.2 GOVERNING EQUATIONS FOR QUASI-ONE-DIMENSIONAL FLOW 620 10.3 NOZZLE
FLOWS 629 10.3.1 MORE ON MASS FLOW 643 10.4 DIFFUSERS 644 10.5
SUPERSONIC WIND TUNNELS 646 10.6 VISCOUS FLOW: SHOCK-WAVE/
BOUNDARY-LAYER INTERACTION INSIDE NOZZLES 652 10.7 SUMMARY 654 10.8
PROBLEMS 655 CONTENTS CHAPTER 11 SUBSONIC COMPRESSIBLE FLOW OVER
AIRFOILS: LINEAR THEORY 657 11.1 INTRODUCTION 658 11.2 THE VELOCITY
POTENTIAL EQUATION 660 11.3 THE LINEARIZED VELOCITY POTENTIAL EQUATION
663 11.4 PRANDTL-GLAUERT COMPRESSIBILITY CORRECTION 668 11.5 IMPROVED
COMPRESSIBILITY CORRECTIONS 673 11.6 CRITICAL MACH NUMBER 674 11.6.1 A
COMMENT ON THE LOCATION OF MINIMUM PRESSURE (MAXIMUM VELOCITY) 683 11.7
DRAG-DIVERGENCE MACH NUMBER: THE SOUND BARRIER 683 11.8 THE AREA RULE
691 11.9 THE SUPERCRITICAL AIRFOIL 693 11.10 CFD APPLICATIONS: TRANSONIC
AIRFOILS AND WINGS 695 11.11 HISTORICAL NOTE: HIGH-SPEED AIRFOILS*EARLY
RESEARCH AND DEVELOPMENT 700 11.12 HISTORICAL NOTE: RICHARD T. WHITCOMB*
ARCHITECT OF THE AREA RULE AND THE SUPERCRITICAL WING 704 11.13 SUMMARY
706 11.14 PROBLEMS 707 CHAPTER 12 LINEARIZED SUPERSONIC FLOW 709 12.1
INTRODUCTION 710 12.2 DERIVATION OF THE LINEARIZED SUPERSONIC PRESSURE
COEFFICIENT FORMULA 710 12.3 APPLICATION TO SUPERSONIC AIRFOILS 714 12.4
VISCOUS FLOW: SUPERSONIC AIRFOIL DRAG 720 12.5 SUMMARY 723 12.6 PROBLEMS
724 CHAPTER 13 INTRODUCTION TO NUMERICAL TECHNIQUES FOR NONLINEAR
SUPERSONIC FLOW 725 13.1 INTRODUCTION: PHILOSOPHY OF COMPUTATIONAL FLUID
DYNAMICS 726 13.2 ELEMENTS OF THE METHOD OF CHARACTERISTICS 728 13.2.1
INTERNAL POINTS 734 13.2.2 WALL POINTS 735 13.3 SUPERSONIC NOZZLE DESIGN
736 13.4 ELEMENTS OF FINITE-DIFFERENCE METHODS 739 13.4.1 PREDICTOR STEP
745 13.4.2 CORRECTOR STEP 745 13.5 THE TIME-DEPENDENT TECHNIQUE:
APPLICATION TO SUPERSONIC BLUNT BODIES 746 13.5.1 PREDICTOR STEP 750
13.5.2 CORRECTOR STEP 750 13.6 SUMMARY 754 13.7 PROBLEM 754 CHAPTER 14
ELEMENTS OF HYPERSONIC FLOW 757 14.1 INTRODUCTION 758 14.2 QUALITATIVE
ASPECTS OF HYPERSONIC FLOW 759 14.3 NEWTONIAN THEORY 763 14.4 THE LIFT
AND DRAG OF WINGS AT HYPERSONIC SPEEDS: NEWTONIAN RESULTS FOR A FLAT
PLATE AT ANGLE OF ATTACK 767 14.4.1 ACCURACY CONSIDERATIONS 774 14.5
HYPERSONIC SHOCK-WAVE RELATIONS AND ANOTHER LOOK AT NEWTONIAN THEORY 778
14.6 MACH NUMBER INDEPENDENCE 782 14.7 HYPERSONICS AND COMPUTATIONAL
FLUID DYNAMICS 784 14.8 SUMMARY 787 14.9 PROBLEMS 787 XVI CONTENTS PART
*T VISCOUS FLOW 789 CHAPTER 15 INTRODUCTION TO THE FUNDAMENTAL
PRINCIPLES AND EQUATIONS OF VISCOUS FLOW 791 15.1 INTRODUCTION 792 15.2
QUALITATIVE ASPECTS OF VISCOUS FLOW 793 15.3 VISCOSITY AND THERMAL
CONDUCTION 801 15.4 THE NAVIER-STOKES EQUATIONS 806 15.5 THE VISCOUS
FLOW ENERGY EQUATION 810 15.6 SIMILARITY PARAMETERS 814 15.7 SOLUTIONS
OF VISCOUS FLOWS: A PRELIMINARY DISCUSSION 818 15.8 SUMMARY 821 15.9
PROBLEMS 823 CHAPTER 16 SOME SPECIAL CASES; COUETTE AND POISEUILLE FLOWS
825 16.1 INTRODUCTION 825 16.2 COUETTE FLOW: GENERAL DISCUSSION 826 16.3
INCOMPRESSIBLE (CONSTANT PROPERTY) COUETTE FLOW 830 16.3.1 NEGLIGIBLE
VISCOUS DISSIPATION 836 16.3.2 EQUAL WALL TEMPERATURES 837 16.3.3
ADIABATIC WALL CONDITIONS (ADIABATIC WALL TEMPERATURE) 839 16.3.4
RECOVERY FACTOR 842 16.3.5 REYNOLDS ANALOGY 843 16.3.6 INTERIM SUMMARY
844 16.4 COMPRESSIBLE COUETTE FLOW 846 16.4.1 SHOOTING METHOD 848 16.4.2
TIME-DEPENDENT FINITE-DIFFERENCE METHOD 850 16.4.3 RESULTS FOR
COMPRESSIBLE COUETTE FLOW 854 16.4.4 SOME ANALYTICAL CONSIDERATIONS 856
16.5 TWO-DIMENSIONAL POISEUILLE FLOW 861 16.6 SUMMARY 865 16.6.1 COUETTE
FLOW 865 16.6.2 POISEUILLE FLOW 865 CHAPTER 17 INTRODUCTION TO BOUNDARY
LAYERS 867 17.1 INTRODUCTION 868 17.2 BOUNDARY-LAYER PROPERTIES 870 17.3
THE BOUNDARY-LAYER EQUATIONS 876 17.4 HOW DO WE SOLVE THE BOUNDARY-LAYER
EQUATIONS? 879 17.5 SUMMARY 881 CHAPTER 18 LAMINAR BOUNDARY LAYERS 883
18.1 INTRODUCTION 883 18.2 INCOMPRESSIBLE FLOW OVER A FLAT PLATE: THE
BLASIUS SOLUTION 884 18.3 COMPRESSIBLE FLOW OVER A FLAT PLATE 891 18.3.1
A COMMENT ON DRAG VARIATION WITH VELOCITY 902 18.4 THE REFERENCE
TEMPERATURE METHOD 903 18.4.1 RECENT ADVANCES: THE MEADOR-SMART
REFERENCE TEMPERATURE METHOD 906 18.5 STAGNATIO N POINT AERODYNAMIC
HEATING 907 18.6 BOUNDARY LAYERS OVER ARBITRARY BODIES:
FINITE-DIFFERENCE SOLUTION 913 18.6.1 FINITE-DIFFERENCE METHOD 914 18.7
SUMMARY 919 18.8 PROBLEMS 920 CHAPTER 19 TURBULENT BOUNDARY LAYERS 921
19.1 INTRODUCTION 922 19.2 RESULTS FOR TURBULENT BOUNDARY LAYERS ON A
FLAT PLATE 922 CONTENTS XVII 19.2.1 REFERENCE TEMPERATURE METHOD FOR
TURBULENT FLOW 924 19.2.2 THE MEADOR-SMART REFERENCE TEMPERATURE METHOD
FOR TURBULENT FLOW 926 19.2.3 PREDICTION OF AIRFOIL DRAG 927 19.3
TURBULENCE MODELING 927 19.3.1 THE BALDWIN-LOMAX MODEL 928 19.4 FINAL
COMMENTS 930 19.5 SUMMARY 931 19.6 PROBLEMS 932 CHAPTER 20 NAVIER-STOKES
SOLUTIONS: SOME EXAMPLES 933 20.1 INTRODUCTION 934 20.2 THE APPROACH 934
20.3 EXAMPLES OF SOME SOLUTIONS 935 20.3.1 FLOW OVER A REARWARD-FACING
STEP 935 20.3.2 FLOW OVER AN AIRFOIL 935 20.3.3 FLOW OVER A COMPLETE
AIRPLANE 938 20.3.4 SHOCK-WAVE/BOUNDARY-LAYER INTERACTION 939 20.3.5
FLOW OVER AN AIRFOIL WITH A PROTUBERANCE 940 20.4 THE ISSUE OF ACCURACY
FOR THE PREDICTION OF SKIN FRICTION DRAG 942 20.5 SUMMARY 947 APPENDIX A
ISENTROPIC FLOW PROPERTIES 949 APPENDIX B NORMAL SHOCK PROPERTIES 955
APPENDIX C PRANDTL-MEYER FUNCTION AND MACH ANGLE 959 APPENDIX D STANDARD
ATMOSPHERE, SI UNITS 963 APPENDIX E STANDARD ATMOSPHERE, ENGLISH
ENGINEERING UNITS 973 BIBLIOGRAPHY 981 INDEX 987 |
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| dewey-search | 629.132/3 |
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| discipline | Physik Verkehrstechnik Verkehr / Transport |
| discipline_str_mv | Physik Verkehrstechnik Verkehr / Transport |
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| index_date | 2024-07-02T15:51:01Z |
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| language | English |
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| spelling | Anderson, John David 1937- Verfasser (DE-588)129741507 aut Fundamentals of aerodynamics John D. Anderson 4. ed. New York, NY [u.a.] McGraw-Hill Higher Education 2007 XXIV, 1008 S. Ill., graph. Darst. 24 cm txt rdacontent n rdamedia nc rdacarrier McGraw-Hill series in aeronautical and aerospace engineering Includes bibliographical references (p. 981-985) and index Aerodinâmica larpcal Aérodynamique Aerodynamics Aerodynamik (DE-588)4000589-6 gnd rswk-swf (DE-588)4123623-3 Lehrbuch gnd-content Aerodynamik (DE-588)4000589-6 s DE-604 http://www.loc.gov/catdir/toc/ecip0513/2005015910.html Table of contents only http://www.loc.gov/catdir/enhancements/fy0634/2005015910-d.html Publisher description HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015023429&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Anderson, John David 1937- Fundamentals of aerodynamics Aerodinâmica larpcal Aérodynamique Aerodynamics Aerodynamik (DE-588)4000589-6 gnd |
| subject_GND | (DE-588)4000589-6 (DE-588)4123623-3 |
| title | Fundamentals of aerodynamics |
| title_auth | Fundamentals of aerodynamics |
| title_exact_search | Fundamentals of aerodynamics |
| title_exact_search_txtP | Fundamentals of aerodynamics |
| title_full | Fundamentals of aerodynamics John D. Anderson |
| title_fullStr | Fundamentals of aerodynamics John D. Anderson |
| title_full_unstemmed | Fundamentals of aerodynamics John D. Anderson |
| title_short | Fundamentals of aerodynamics |
| title_sort | fundamentals of aerodynamics |
| topic | Aerodinâmica larpcal Aérodynamique Aerodynamics Aerodynamik (DE-588)4000589-6 gnd |
| topic_facet | Aerodinâmica Aérodynamique Aerodynamics Aerodynamik Lehrbuch |
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