Holdings: Analysis of low-speed unsteady airfoil flows

Analysis of low-speed unsteady airfoil flows: with 3 tables, and a CD-ROM

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Bibliographic Details
Format:	Book
Language:	English
Published:	Berlin [u.a.] Springer [u.a.] 2005
Subjects:	Instationäre Strömung Numerische Strömungssimulation Tragflügelumströmung
Online Access:	Inhaltsverzeichnis
Physical Description:	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

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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 NAVIERSTOKES 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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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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