Analysis of low-speed unsteady airfoil flows: with 3 tables, and a CD-ROM
Gespeichert in:
| Format: | Buch |
|---|---|
| Sprache: | English |
| Veröffentlicht: |
Berlin [u.a.]
Springer [u.a.]
2005
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XII, 226 S. Ill., graph. Darst. 1 CD-ROM (12 cm) |
| Format: | Systemvoraussetzungen:. - Operating system: Win95, Win98, WinME, WinNT 4.0, Win2000, WinXP or UNIX, Linux. Web browser: Internet explorer 5.5 (or higher) or Netscape 4.7 (or higher). Adobe Acrobat Reader 4.0 (or higher). UNIX FORTRAN compiler if using UNIX. Since PC executable files are on the CD-ROM, it does not require PC compiler. |
| ISBN: | 0966846184 |
Internformat
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Datensatz im Suchindex
| _version_ | 1804139003775025152 |
|---|---|
| adam_text | TUNCERCEBECI MAX PLATZER HSUN CHEN KUO-CHENG CHANG JIAN P. SHAO ANALYSIS
OF LOW-SPEED UNSTEADY AIRFOIL FLOWS WITH 131 FIGURES, 3 TABLES, AND A
CD-ROM * *- *LX _ SPRINGER HORIZONS PUBLISHING CONTENTS 1. PHYSICS OF
UNSTEADY FLOWS 1 1.1 INTRODUCTION 1 1.2 LIFT GENERATION 5 1.3 THRUST
GENERATION BY AIRFOIL OSCILLATION 8 1.4 POWER EXTRACTION 10 1.5
SINGLE-DEGREE-OF-FREEDOM AIRFOIL FLUTTER 13 1.6 AIRFOIL GUST RESPONSE 15
1.7 DYNAMIC AIRFOIL STALL 16 1.8 STALL FLUTTER 18 1.9 SUMMARY 19
REFERENCES 19 2. THE DIFFERENTIAL EQUATIONS OF FLUID FLOW 21 2.1
INTRODUCTION 21 2.2 NAVIER-STOKES EQUATIONS 22 2.3 REYNOLDS-AVERAGED
NAVIER*STOKES EQUATIONS 24 2.4 REDUCED FORMS OF THE NAVIER-STOKES
EQUATIONS . . 25 2.4.1 PARABOLIZED AND THIN-LAYER NAVIER-STOKES
EQUATIONS ... 25 2.4.2 INVISCID FLOW EQUATIONS ,. . 26 2.4.3
BOUNDARY-LAYER EQUATIONS 27 REFERENCES 29 3. PANEL METHODS 31 3.1
INTRODUCTION 31 3.2 HSPM. . ... 31 3.3 EXTENSION OF HSPM TO UNSTEADY
AIRFOIL FLOWS 38 3.3.1 INFLUENCE COEFFICIENTS 40 3.3.2 SOLUTION
PROCEDURE 42 3.3.3 VELOCITY POTENTIAL AND PRESSURE DISTRIBUTION 45 X
CONTENTS 3.4 EXTENSION OF HSPM TO UNSTEADY FLOW OVER FINITE-SPAN WINGS .
47 REFERENCES 47 4. APPLICATIONS OF PANEL METHOD 49 4.1 INTRODUCTION 49
4.2 ANALYSIS OF LIFT GENERATION 49 4.3 ANALYSIS OF THRUST GENERATION OR
POWER EXTRACTION 53 4.4 ANALYSIS OF OSCILLATING AIRFOILS 54 4.5 ANALYSIS
OF TORSIONAL AIRFOIL FLUTTER 56 4.6 ANALYSIS OF AIRFOIL GUST RESPONSE 57
REFERENCES 58 5. BOUNDARY-LAYER METHODS 59 5.1 INTRODUCTION 59 5.2
STANDARD, INVERSE AND INTERACTION PROBLEMS 61 5.2.1 STANDARD PROBLEM 61
5.2.2 INVERSE PROBLEM 62 5.2.3 INTERACTION PROBLEM 63 5.3 SOLUTION OF
THE STANDARD PROBLEM FOR TWO-DIMENSIONAL STEADY FLOWS . 64 5.3.1
NUMERICAL FORMULATION 66 5.3.2 NEWTON S METHOD 69 5.3.3
BLOCK-ELIMINATION METHOD 71 5.4 SOLUTION OF THE INVERSE PROBLEM FOR
TWO-DIMENSIONAL STEADY FLOWS 72 5.5 SOLUTION OF THE STANDARD AND INVERSE
PROBLEMS FOR TWO-DIMENSIONAL UNSTEADY FLOWS 76 5.5.1 INITIAL CONDITIONS
77 5.5.2 TRANSFORMED EQUATIONS 78 5.5.3 NUMERICAL METHOD: FLOWS WITHOUT
REVERSAL * 79 5.5.4 NUMERICAL METHOD: FLOWS WITH REVERSAL . * 83
REFERENCES 91 6. APPLICATIONS OF BOUNDARY-LAYER METHODS: FLOWS WITHOUT
SEPARATION 93 6.1 INTRODUCTION 93 6.2 UNSTEADY BOUNDARY-LAYERS WITH
FLUCTUATIONS IN EXTERNAL VELOCITY 93 6.2.1 LAMINAR FLOWS 93 6.2.2
TURBULENT FLOWS 96 6.3 BOUNDARY-LAYER MOTION STARTED IMPULSIVELY FROM
REST 97 6.3.1 IMPULSIVELY STARTED FLAT PLATE 97 CONTENTS XI 6.3.2
IMPULSIVELY STARTED CIRCULAR CYLINDER: UNSTEADY SEPARATION 99
REFERENCES 103 7. APPLICATIONS OF BOUNDARY-LAYER METHODS: FLOWS WITH
SEPARATION 105 7.1 INTRODUCTION 105 7.2 SEPARATION AND REATTACHMENT NEAR
THE LEADING EDGE OF A THIN OSCILLATING AIRFOIL 106 7.2.1 MODEL PROBLEM
106 7.2.2 INITIAL CONDITIONS 108 7.2.3 THE QUESTION OF SINGULARITY ON AN
OSCILLATING AIRFOIL. . . . 112 7.2.4 INTERACTION AS AN ANSWER TO THE
QUESTION OF SINGULARITY . 118 7.3 STEADY AIRFOIL FLOWS 123 7.3.1
AIRFOILS AT LOW REYNOLDS NUMBERS 125 7.3.2 AIRFOILS AT HIGH REYNOLDS
NUMBERS 130 7.4 UNSTEADY AIRFOIL FLOWS 133 7.4.1 RESULTS OF UNSTEADY
FLOWS 139 7.4.2 INITIATION OF DYNAMIC STALL ON A PITCHING AIRFOIL 148
7.4.3 SUMMARY 149 REFERENCES 151 8. NAVIER-STOKES METHODS 153 8.1
INTRODUCTION 153 8.2 NAVIER-STOKES EQUATIONS 154 8.2.1 VECTOR-VARIABLE
FORM 156 8.2.2 TRANSFORMED FORM 158 8.3 TURBULENCE MODELS 161 8.3.1
ALGEBRAIC MODELS 162 8.3.2 ONE-EQUATION MODELS - 166 8.3.3 TWO-EQUATION
MODELS 167 8.4 NUMERICAL METHODS: INCOMPRESSIBLE FLOWS 172 8.4.1
VORTICITY-STREAMFUNCTION FORMULATION 173 8.4.2 VELOCITY-VORTICITY
FORMULATION 173 8.4.3 PSEUDO-COMPRESSIBILITY FORMULATION 175 8.5
NUMERICAL METHODS: COMPRESSIBLE FLOWS 181 REFERENCES 188 9. APPLICATIONS
OF NAVIER*STOKES METHODS 191 9.1 INTRODUCTION 191 9.2 LAMINAR FLOW
CALCULATIONS FOR INCOMPRESSIBLE FLOWS 192 9.3 LAMINAR FLOW CALCULATIONS
FOR COMPRESSIBLE FLOWS 192 XII CONTENTS 9.4 LAMINAR AND TURBULENT FLOW
CALCULATIONS FOR INCOMPRESSIBLE AND COMPRESSIBLE FLOWS 196 9.5 EFFECT OF
TRANSITION 200 9.6 FLAPPING-WING FLIGHT 204 9.7 THREE-DIMENSIONAL
DYNAMIC STALL CALCULATIONS 206 REFERENCES 208 10. COMPANION COMPUTER
PROGRAMS 211 10.1 INTRODUCTION 211 10.2 HESS-SMITH PANEL METHOD (HSPM)
FOR STEADY FLOWS 211 10.3 INTERACTIVE BOUNDARY-LAYER PROGRAM 212 10.3.1
INPUT 213 10.3.2 OUTPUT 214 10.3.3 TEST CASES 215 REFERENCES 223 SUBJECT
INDEX 225
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| indexdate | 2024-07-09T21:37:11Z |
| institution | BVB |
| isbn | 0966846184 |
| language | English |
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| physical | XII, 226 S. Ill., graph. Darst. 1 CD-ROM (12 cm) |
| publishDate | 2005 |
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| spelling | Analysis of low-speed unsteady airfoil flows with 3 tables, and a CD-ROM Tuncer Cebeci ... Berlin [u.a.] Springer [u.a.] 2005 XII, 226 S. Ill., graph. Darst. 1 CD-ROM (12 cm) txt rdacontent n rdamedia nc rdacarrier Systemvoraussetzungen:. - Operating system: Win95, Win98, WinME, WinNT 4.0, Win2000, WinXP or UNIX, Linux. Web browser: Internet explorer 5.5 (or higher) or Netscape 4.7 (or higher). Adobe Acrobat Reader 4.0 (or higher). UNIX FORTRAN compiler if using UNIX. Since PC executable files are on the CD-ROM, it does not require PC compiler. Instationäre Strömung (DE-588)4132734-2 gnd rswk-swf Numerische Strömungssimulation (DE-588)4690080-9 gnd rswk-swf Tragflügelumströmung (DE-588)4185837-2 gnd rswk-swf Tragflügelumströmung (DE-588)4185837-2 s Instationäre Strömung (DE-588)4132734-2 s Numerische Strömungssimulation (DE-588)4690080-9 s DE-604 Cebeci, Tuncer Sonstige oth HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=017446673&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Analysis of low-speed unsteady airfoil flows with 3 tables, and a CD-ROM Instationäre Strömung (DE-588)4132734-2 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Tragflügelumströmung (DE-588)4185837-2 gnd |
| subject_GND | (DE-588)4132734-2 (DE-588)4690080-9 (DE-588)4185837-2 |
| title | Analysis of low-speed unsteady airfoil flows with 3 tables, and a CD-ROM |
| title_auth | Analysis of low-speed unsteady airfoil flows with 3 tables, and a CD-ROM |
| title_exact_search | Analysis of low-speed unsteady airfoil flows with 3 tables, and a CD-ROM |
| title_full | Analysis of low-speed unsteady airfoil flows with 3 tables, and a CD-ROM Tuncer Cebeci ... |
| title_fullStr | Analysis of low-speed unsteady airfoil flows with 3 tables, and a CD-ROM Tuncer Cebeci ... |
| title_full_unstemmed | Analysis of low-speed unsteady airfoil flows with 3 tables, and a CD-ROM Tuncer Cebeci ... |
| title_short | Analysis of low-speed unsteady airfoil flows |
| title_sort | analysis of low speed unsteady airfoil flows with 3 tables and a cd rom |
| title_sub | with 3 tables, and a CD-ROM |
| topic | Instationäre Strömung (DE-588)4132734-2 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Tragflügelumströmung (DE-588)4185837-2 gnd |
| topic_facet | Instationäre Strömung Numerische Strömungssimulation Tragflügelumströmung |
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