Foundations of aerodynamics:
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Book |
| Language: | English |
| Published: |
New York
Wiley [u.a.]
1959
|
| Edition: | 2. ed. |
| Subjects: | |
| Online Access: | Inhaltsverzeichnis |
| Physical Description: | XIV, 446 S. |
Staff View
MARC
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| 100 | 1 | |a Kuethe, Arnold M. |d 1905- |e Verfasser |0 (DE-588)172200474 |4 aut | |
| 245 | 1 | 0 | |a Foundations of aerodynamics |c A. M. Kuethe ; J. D. Schetzer |
| 250 | |a 2. ed. | ||
| 264 | 1 | |a New York |b Wiley [u.a.] |c 1959 | |
| 300 | |a XIV, 446 S. | ||
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| 700 | 1 | |a Schetzer, Julius D. |e Verfasser |4 aut | |
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Record in the Search Index
| _version_ | 1804140072362049536 |
|---|---|
| adam_text | Contents
Chapter 1 The Fluid Medium 1
1 1 INTRODUCTION 1
1 2 PROPERTIES OF GASES AT REST 1
1 3 STANDARD ATMOSPHERE 3
1 4 GASES IN MOTION—VISCOSITY 3
1 5 DISSIPATION OF ENERGY 5
1 6 INTERPRETATION OF THE COEFFICIENT OF
VISCOSITY AND THERMAL CONDUCTIVITY 6
1 7 FORCE ON A BODY MOVING THROUGH A
FLUID 9
1 8 THE APPROXIMATE FORMULATION OF FLOW
PROBLEMS 11
1 9 PLAN FOR THE FOLLOWING CHAPTERS 12
Chapter 2 Kinematics of a Fluid Field 13
2 1 FIELDS 13
2 2 SCALAR FIELD, DIRECTIONAL DERIVATIVE,
GRADIENT 13
2 3 VECTOR FIELD—METHOD OF DESCRIPTION 16
2 4 DIVERGENCE OF A VECTOR, THEOREM OF
GAUSS 19
2 5 CONSERVATION OF MASS AND THE EQUATION
OF CONTINUITY 21
2 6 STREAM FUNCTION IN TWO-DIMENSIONAL
INCOMPRESSIBLE FLOW 24
2 7 THE SHEARING DERIVATIVES-ROTATION AND
STRAIN 25
2 8 CIRCULATION, CURL OF A VECTOR 28
2 9 IRROTATIONAL FLOW 32
2 10 THEOREM OF STOKES 34
2 11 VELOCITY POTENTIAL 36
ix
CONTENTS
Chapter 2
Chapter 3
Chapter 4
Chapter 5
Chapter 6
2 12 POINT VORTEX, VORTEX FILAMENT, LAW OF
BIOT AND SAVART 38
2 13 VORTEX SHEETS 39
2 14 HELMHOLTZ’ VORTEX THEOREMS 41
Dynamics of a Fluid Field
3 1 ACCELERATION 43
3 2 euleb’s equation 45
3 3 the momentum theorem of fluid
MECHANICS 47
3 4 Bernoulli’s equation 51
3 5 Bernoulli’s equation for irrotational
flow 54
The Flow about a Body
4 1 introduction 57
4 2 superposition of flows 59
4 3 SOURCE flow 60
4 4 FLOW PATTERN OF A SOURCE AND SINK OF
EQUAL STRENGTH-DOUBLET 62
4 5 FLOW ABOUT A CYLINDER IN A UNIFORM
STREAM 64
4 6 VORTEX FLOW—CIRCULATORY FLOW ABOUT A
CYLINDER 65
4 7 CIRCULATORY FLOW ABOUT A CYLINDER IN A
UNIFORM STREAM- 66
4 8 FORCE ON A CYLINDER WITH CIRCULATION IN A
UNIFORM STREAM 67
4 9 KUTTA-JOUKOWSKI THEOREM 69
4 10 BOUND VORTEX 72
4 11 KUTTA CONDITION 72
The Thin Airfoil
5 1 INTRODUCTION 75
5 2 THE VORTEX SHEET IN THIN-AIRFOIL THEORY 76
5 3 PLANAR WING 80
5 4 PROPERTIES OF THE SYMMETRICAL AIRFOIL 80
5 5 VORTICITY DISTRIBUTION FOR THE CAMBERED
AIRFOIL 83
5 6 PROPERTIES OF THE CAMBERED AIRFOIL 85
5 7 INFLUENCE OF CAMBER ON aLO AND Cm« 88
5 8 THE FLAPPED AIRFOIL 90
5 9 CONCLUDING REMARKS 93
Finite Wing
6 1 INTRODUCTION 94
6 2 BOUND VORTICITY 94
6 3 HORSESHOE VORTEX SYSTEM 97
6 4 THE FIELD OF FLOW—DOWNWASH AND INDUCED
DRAG 99
Chapter 6
Chapter 7
Chapter 8
Chapter 9
CONTENTS xi
6 5 FUNDAMENTAL EQUATION OF FINITE-WING
THEORY 102
6 6 THE ELLIPTICAL LIFT DISTRIBUTION 104
6 7 GLAUERt’s SOLUTION OF THE FUNDAMENTAL
equation 107
6 8 WING AND SECTION PROPERTIES IN TERMS OF THE
dn’s OF GLAUERT’S SOLUTION 109
6 9 THE TWISTED WING—BASIC AND ADDITIONAL
LIFT 111
6 10 FIRST-ORDER EFFECT OF DEVIATION FROM AN
ELLIPTIC DISTRIBUTION 114
6 11 ADDITIONAL CHARACTERISTICS OF THE FINITE
WING 115
6 12 STABILITY AND TRIM OF WINGS 117
6 13 APPROXIMATIONS IN PRANDTL LIFTING LINE
THEORY 119
6 14 CONCLUDING REMARKS 121
Introduction to Compressible Fluids 123
7 1 scope 123
7 2 EQUATION OF CONTINUITY—STREAM FUNCTION 124
7 3 IRROTATIONALITY—VELOCITY POTENTIAL 125
7 4 EQUATION OF EQUILIBRIUM—BERNOULLI’S
EQUATION 126
7 5 NONSUPERPOSITION OF COMPRESSIBLE FLOWS 126
The Energy Relations 128
8 1 INTRODUCTION 128
8 2 CHARACTERISTICS OF AN IDEAL GAS—EQUATION
OF STATE 129
8 3 FIRST LAW OF THERMODYNAMICS 133
8 4 STEADY FLOW ENEBGY EQUATION 136
8 5 REVERSIBILITY 140
8 6 SECOND LAW OF THERMODYNAMICS 142
8 7 Bernoulli’s equation for isentropic
COMPRESSIBLE FLOW 144
8 8 STATIC AND STAGNATION VALUES 146
Some Applications of One-Dimensional
Compressible Flow 148
9 1 INTRODUCTION 148
9 2 SPEED OF SOUND 148
9 3 ISENTROPIC FLOW RELATIONS IN TERMS OF MACH
NUMBER 152
9 4 MEASUREMENT OF FLIGHT SPEED (SUBSONIC) 154
9 5 ISENTROPIC ONE-DIMENSIONAL FLOW 154
9 6 THE LAVAL NOZZLE 156
9 7 ONE-DIMENSIONAL FLOW WITH FRICTION AND
HEAT ADDITION 159
9 8 HEAT ADDITION TO A CONSTANT AREA DUCT 161
xii
Chapter 10
Chapter 11
Chapter 12
Chapter 13
CONTENTS
Waves 165
10 1 ESTABLISHMENT OF A FLOW FIELD 165
10 2 MACH WAVES 167
10 3 LARGE AMPLITUDE WAVES 169
10 4 PRANDTL-MEYER FLOW 171
10 5 FINITE COMPRESSION WAVES 174
10 6 THE CHARACTERISTIC RATIOS AS FUNCTIONS OF
MACH NUMBER 179
10 7 NORMAL SHOCK WAVE 182
10 8 PLANE OBLIQUE SHOCK WAVES 183
10 9 CONICAL OBLIQUE SHOCK WAVES 185
10 10 SHOCKS IN TUBES 189
10 11 REFLECTION OF WAVES 191
Wings in Compressible Flow 192
11 1 INTRODUCTION 192
11 2 THE FLOW EQUATION 193
11 3 FLOW EQUATION FOR SMALL PERTURBATIONS 195
11 4 THE PRESSURE COEFFICIENT FOR SMALL
PERTURBATIONS 197
11 5 LIFTING AND NONLIFTING COMPONENTS—BOUNDARY
CONDITIONS 198
11 6 PLANAR WINGS IN SUBSONIC FLOW—PRANDTL-
GLAUERT TRANSFORMATION 200
11 7 THE CRITICAL MACH NUMBER OF AN AIRFOIL 203
11 8 THE THIN WING IN SUPERSONIC FLOW 206
11 9 THE SUPERSONIC SOURCE 208
11 10 THE NONLIFTING PROBLEM 211
11 11 THE LIFTING PROBLEM—SUPERSONIC EDGES 213
11 12 THE LIFTING PROBLEM-SUBSONIC EDGES 216
11 13 SECTION CHARACTERISTICS FOR THE INFINITE
SUPERSONIC WING 217
11 14 INFLUENCE OF SWEEP ON DRAG 221
The Dynamics of Viscous Fluids 223
12 1 INTRODUCTION 223
12 2 THE NO-SLIP CONDITION 225
12 3 THE BOUNDARY LAYER 225
12 4 viscous stresses 227
12 5 BOUNDARY LAYER EQUATION OF MOTION 228
12 6 SIMILARITY IN INCOMPRESSIBLE FLOWS 230
Incompressible Laminar Flow in Tubes and
Boundary Layers 232
13 1 INTRODUCTION 232
13 2 LAMINAR FLOW IN A TUBE 232
13 3 LAMINAR BOUNDARY LAYER ALONG A FLAT
PLATE 234
13 4 FLOW WITH PRESSURE GRADIENT—SEPARATION 241
u
;
3 3
II
CONTENTS
Chapter 13
Chapter 14
Chapter 15
Chapter 16
xiii
13 5 SIMILARITY IN BOUNDARY LAYER FLOWS 243
13 6 THE VON KARMAN INTEGRAL RELATION 245
13 7 THE POHLHAUSEN ANALYSIS OF THE BOUNDARY
LAYER 248
13 8 THREE-DIMENSIONAL BOUNDARY LAYERS 251
Laminar Boundary Layer in Compressible Flow 255
14 1 INTRODUCTION 255
14 2 CONSERVATION OF ENERGY IN THE BOUNDARY
LAYER 256
14 3 ROTATION AND ENTROPY GRADIENT IN THE BOUNDARY
LAYER 259
14 4 SIMILARITY CONSIDERATIONS FOR COMPRESSIBLE
BOUNDARY LAYERS 260
14 5 SOLUTIONS OF THE ENERGY EQUATION FOR PRANDTL
NUMBER UNITY 261
14 6 TEMPERATURE RECOVERY FACTOR 265
14 7 heat transfer versus skin friction 268
14 8 VELOCITY AND TEMPERATURE PROFILES AND SKIN
FRICTION 271
14 9 EFFECTS OF PRESSURE GRADIENT 273
Transition from Laminar to Turbulent Flow 278
15 1 INTRODUCTION 278
15 2 DESCRIPTION OF TURBULENT FLOW 279
15 3 METHOD OF MEASUREMENT OF TURBULENCE 281
15 4 DESCRIPTION OF TRANSITION 282
15 5 FACTORS AFFECTING TRANSITION 287
15 6 METHODS FOR EXPERIMENTALLY DETECTING
transition 296
15 7 FLOW AROUND SPHERES AND CIRCULAR
CYLINDERS 298
Turbulent Flow in Tubes and Boundary Layers 302
16 1 INTRODUCTION 302
16 2 QUANTITATIVE DESCRIPTION OF TURBULENCE 302
16 3 TURBULENT SHEARING STRESS 304
16 4 BOUNDARY LAYER EQUATION FOR TURBULENT
FLOW 306
16 5 THE MIXING-LENGTH HYPOTHESIS 308
16 6 FULLY DEVELOPED FLOW IN A TUBE 309
16 7 THE TURBULENT BOUNDARY LAYER ON A FLAT
PLATE 313
16 8 SIMILARITY CONSIDERATIONS 315
16 9 EFFECTS OF SURFACE ROUGHNESS 318
16 10 TURBULENT BOUNDARY LAYER IN A PRESSURE
GRADIENT—FLOW SEPARATION 321
16 11 EFFECTS OF COMPRESSIBILITY 323
16 12 REYNOLDS ANALOGY—HEAT TRANSFER AND
TEMPERATURE RECOVERY FACTOR 325
xiv
CONTENTS
Appendix A Dimensional Analysis 327
Appendix B Derivation of the Navier-Stokes and the Energy
Equations 332
1 INTRODUCTION 332
2 PRINCIPAL, AXES 334
3 TRANSFORMATION EQUATIONS 335
4 THE STRESSES AT A POINT 337
5 CONSERVATION OF MOMENTUM—NAVIER-STOKES
EQUATIONS 340
6 CONSERVATION OF ENERGY 342
7 BOUNDARY LAYER EQUATIONS 345
Appendix C Aerodynamic Characteristics of Wings 351
1 INTRODUCTION 351
2 CHARACTERISTICS OF WING SECTIONS AT LOW
SPEEDS 352
3 HIGH SUBSONIC AND TRANSONIC EFFECTS 359
4 WINGS AT SUPERSONIC SPEEDS 361
5 CHARACTER OF THE STALL FOR INCOMPRESSIBLE
FLOW 366
6 MAXIMUM LIFT COEFFICIENT 368
7 STALL OF FINITE WINGS 371
8 EFFECTS OF SWEEP 372
Appendix D Real Fluid Effects in High-Speed Flight 376
1 INTRODUCTION-MODEL OF A GAS 376
2 FLOW REGIMES FOR REAL GASES AT ORDINARY
TEMPERATURES 377
3 NEWTONIAN FLOW 382
4 SOME ASPECTS OF HIGH-TEMPERATURE FLOWS 383
Problems 391
Tables 415
1 PROPERTIES OF THE STANDARD ATMOSPHERE 416
2 FLOW PARAMETERS VERSUS M FOR SUBSONIC
FLOW 417
3 FLOW PARAMETERS VERSUS M FOR SUPERSONIC
FLOW 420
4 PARAMETERS FOR SHOCK FLOW 429
5 THERMAL PROPERTIES OF GASES 435
Oblique Shock Chart 436
Index 437
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| any_adam_object | 1 |
| author | Kuethe, Arnold M. 1905- Schetzer, Julius D. |
| author_GND | (DE-588)172200474 |
| author_facet | Kuethe, Arnold M. 1905- Schetzer, Julius D. |
| author_role | aut aut |
| author_sort | Kuethe, Arnold M. 1905- |
| author_variant | a m k am amk j d s jd jds |
| building | Verbundindex |
| bvnumber | BV024658816 |
| classification_rvk | UF 4700 |
| ctrlnum | (OCoLC)638056048 (DE-599)BVBBV024658816 |
| discipline | Physik |
| edition | 2. ed. |
| format | Book |
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| indexdate | 2024-07-09T21:54:10Z |
| institution | BVB |
| language | English |
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| physical | XIV, 446 S. |
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| spelling | Kuethe, Arnold M. 1905- Verfasser (DE-588)172200474 aut Foundations of aerodynamics A. M. Kuethe ; J. D. Schetzer 2. ed. New York Wiley [u.a.] 1959 XIV, 446 S. txt rdacontent n rdamedia nc rdacarrier Aerodynamik (DE-588)4000589-6 gnd rswk-swf Aerodynamik (DE-588)4000589-6 s DE-604 Schetzer, Julius D. Verfasser aut HEBIS Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018070018&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Kuethe, Arnold M. 1905- Schetzer, Julius D. Foundations of aerodynamics Aerodynamik (DE-588)4000589-6 gnd |
| subject_GND | (DE-588)4000589-6 |
| title | Foundations of aerodynamics |
| title_auth | Foundations of aerodynamics |
| title_exact_search | Foundations of aerodynamics |
| title_full | Foundations of aerodynamics A. M. Kuethe ; J. D. Schetzer |
| title_fullStr | Foundations of aerodynamics A. M. Kuethe ; J. D. Schetzer |
| title_full_unstemmed | Foundations of aerodynamics A. M. Kuethe ; J. D. Schetzer |
| title_short | Foundations of aerodynamics |
| title_sort | foundations of aerodynamics |
| topic | Aerodynamik (DE-588)4000589-6 gnd |
| topic_facet | Aerodynamik |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018070018&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT kuethearnoldm foundationsofaerodynamics AT schetzerjuliusd foundationsofaerodynamics |