Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Abschlussarbeit Buch |
| Sprache: | English |
| Veröffentlicht: |
Köln
2007
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| Ausgabe: | Als Ms. gedr. |
| Schriftenreihe: | Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt
2007,3 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Zsfassung in dt. Sprache |
| Beschreibung: | VIII, 137 S. Ill., graph. Darst. 21 cm |
Internformat
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Datensatz im Suchindex
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| adam_text | FORSCHUNGSBERICHT 2007-03 NUMERICAL INVESTIGATION OF UNSTEADY TRANSONIC
SHOCK/BOUNDARY-LAYER INTERACTION FOR AERONAUTICAL APPLICATIONS ANTE SODA
GERMAN AEROSPACE CENTER INSTITUTE OF AEROELASTICITY GOTTINGEN 150 SEITEN
98 BILDER 7 TABELLEN 92 LITERATURSTELLEN ULB DARMSTADT ILLILLLLLLLLL
16605786 DEUTSCHES ZENTRUM DLR FUR LUFT- UND RAUMFAHRT E.V IN DER
HELMHOLTZ-GEMEINSCHAFT CONTENTS V CONTENTS LIST OF SYMBOLS VII 1
INTRODUCTION 1 1.1 MOTIVATION FOR RESEARCH 1 1.2 RESEARCH OBJECTIVES 4
1.3 THESIS LAYOUT 5 2 SHOCK-BUFFET PHENOMENA RELEVANT TO AEROFOILS AND
WINGS 6 2.1 PHYSICAL BACKGROUND OF SHOCK-BUFFET 7 2.2 BUFFET MECHANISMS
IN LAMINAR AND TURBULENT BOUNDARY LAYERS 9 2.3 MANIFESTATION AND CONTROL
OF SHOCK-BUFFET 16 3 NUMERICAL MODELLING 19 3.1 THE DLR-TAU CODE 19 3.2
TURBULENCE MODELLING 23 3.3 BEYOND REYNOLDS-AVERAGING 24 3.4 BOUNDARY
CONDITIONS .* 26 4 INVESTIGATION OF SHOCK-BUFFET IN 2-D USING RANS 27
4.1 NACA 64A010 27 4.1.1 AGARD SSC STEADY TEST CASE 28 4.1.2 VARIATION
OF FLOW PARAMETERS 31 4.1.3 AGARD SSC UNSTEADY CALCULATIONS 35 4.1.4
SHOCK-BUFFET RESULTS 39 4.2 NACA 0012 52 4.2.1 STEADY FLOW CONDITIONS 52
4.2.2 SHOCK-BUFFET RESULTS 54 4.2.3 INFLUENCE OF REYNOLDS NUMBER 62 4.3
NLR 7301 63 4.3.1 ANALYSIS OF STEADY FLOW FIELD 64 4.3.2 ANALYSIS OF
BUFFET RESULTS 66 4.3.3 GRID CONVERGENCE STUDY 76 VI CONTENTS 5
INVESTIGATION OF SHOCK-BUFFET IN 3-D USING DES 82 5.1 COMPUTATIONAL
GRIDS FOR DES 82 5.2 ANALYSIS OF DES SHOCK-BUFFET RESULTS 85 5.3
VALIDATION OF CONVECTIVE-ACOUSTIC SHOCK-BUFFET MECHANISM 91 6
SHOCK-BUFFET ON A GENERIC WING/NACELLE MODEL 100 6.1 ABOUT WIONA MODEL
101 6.2 ANALYSIS OF STEADY VISCOUS WING/NACELLE INTERFERENCE 104 6.3
INFLUENCE OF UNSTEADY PITCHING GEOMETRY 115 6.4 SHOCK-BUFFET IN
WING/NACELLE CHANNEL 118 7 CONCLUSIONS 129 REFERENCES 131
|
| adam_txt |
FORSCHUNGSBERICHT 2007-03 NUMERICAL INVESTIGATION OF UNSTEADY TRANSONIC
SHOCK/BOUNDARY-LAYER INTERACTION FOR AERONAUTICAL APPLICATIONS ANTE SODA
GERMAN AEROSPACE CENTER INSTITUTE OF AEROELASTICITY GOTTINGEN 150 SEITEN
98 BILDER 7 TABELLEN 92 LITERATURSTELLEN ULB DARMSTADT ILLILLLLLLLLL
16605786 DEUTSCHES ZENTRUM DLR FUR LUFT- UND RAUMFAHRT E.V IN DER
HELMHOLTZ-GEMEINSCHAFT CONTENTS V CONTENTS LIST OF SYMBOLS VII 1
INTRODUCTION 1 1.1 MOTIVATION FOR RESEARCH 1 1.2 RESEARCH OBJECTIVES 4
1.3 THESIS LAYOUT 5 2 SHOCK-BUFFET PHENOMENA RELEVANT TO AEROFOILS AND
WINGS 6 2.1 PHYSICAL BACKGROUND OF SHOCK-BUFFET 7 2.2 BUFFET MECHANISMS
IN LAMINAR AND TURBULENT BOUNDARY LAYERS 9 2.3 MANIFESTATION AND CONTROL
OF SHOCK-BUFFET 16 3 NUMERICAL MODELLING 19 3.1 THE DLR-TAU CODE 19 3.2
TURBULENCE MODELLING 23 3.3 BEYOND REYNOLDS-AVERAGING 24 3.4 BOUNDARY
CONDITIONS .* 26 4 INVESTIGATION OF SHOCK-BUFFET IN 2-D USING RANS 27
4.1 NACA 64A010 27 4.1.1 AGARD SSC STEADY TEST CASE 28 4.1.2 VARIATION
OF FLOW PARAMETERS 31 4.1.3 AGARD SSC UNSTEADY CALCULATIONS 35 4.1.4
SHOCK-BUFFET RESULTS 39 4.2 NACA 0012 52 4.2.1 STEADY FLOW CONDITIONS 52
4.2.2 SHOCK-BUFFET RESULTS 54 4.2.3 INFLUENCE OF REYNOLDS NUMBER 62 4.3
NLR 7301 63 4.3.1 ANALYSIS OF STEADY FLOW FIELD 64 4.3.2 ANALYSIS OF
BUFFET RESULTS 66 4.3.3 GRID CONVERGENCE STUDY 76 VI CONTENTS 5
INVESTIGATION OF SHOCK-BUFFET IN 3-D USING DES 82 5.1 COMPUTATIONAL
GRIDS FOR DES 82 5.2 ANALYSIS OF DES SHOCK-BUFFET RESULTS 85 5.3
VALIDATION OF CONVECTIVE-ACOUSTIC SHOCK-BUFFET MECHANISM 91 6
SHOCK-BUFFET ON A GENERIC WING/NACELLE MODEL 100 6.1 ABOUT WIONA MODEL
101 6.2 ANALYSIS OF STEADY VISCOUS WING/NACELLE INTERFERENCE 104 6.3
INFLUENCE OF UNSTEADY PITCHING GEOMETRY 115 6.4 SHOCK-BUFFET IN
WING/NACELLE CHANNEL 118 7 CONCLUSIONS 129 REFERENCES 131 |
| any_adam_object | 1 |
| any_adam_object_boolean | 1 |
| author | Soda, Ante |
| author_facet | Soda, Ante |
| author_role | aut |
| author_sort | Soda, Ante |
| author_variant | a s as |
| building | Verbundindex |
| bvnumber | BV022823563 |
| ctrlnum | (OCoLC)611897587 (DE-599)HBZHT015228970 |
| dewey-full | 533.274 |
| dewey-hundreds | 500 - Natural sciences and mathematics |
| dewey-ones | 533 - Pneumatics (Gas mechanics) |
| dewey-raw | 533.274 |
| dewey-search | 533.274 |
| dewey-sort | 3533.274 |
| dewey-tens | 530 - Physics |
| discipline | Physik |
| discipline_str_mv | Physik |
| edition | Als Ms. gedr. |
| format | Thesis Book |
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| index_date | 2024-07-02T18:40:54Z |
| indexdate | 2024-07-09T21:06:58Z |
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| language | English |
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| spelling | Soda, Ante Verfasser aut Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications Ante Soda Als Ms. gedr. Köln 2007 VIII, 137 S. Ill., graph. Darst. 21 cm txt rdacontent n rdamedia nc rdacarrier Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt 2007,3 Zsfassung in dt. Sprache Zugl.: Aachen, Techn. Hochsch., Diss., 2006 Tragflügelumströmung (DE-588)4185837-2 gnd rswk-swf Numerische Strömungssimulation (DE-588)4690080-9 gnd rswk-swf Transsonische Strömung (DE-588)4135633-0 gnd rswk-swf Grenzschichtablösung (DE-588)4136915-4 gnd rswk-swf (DE-588)4113937-9 Hochschulschrift gnd-content Numerische Strömungssimulation (DE-588)4690080-9 s Transsonische Strömung (DE-588)4135633-0 s Tragflügelumströmung (DE-588)4185837-2 s Grenzschichtablösung (DE-588)4136915-4 s DE-604 Deutsches Zentrum für Luft- und Raumfahrt Forschungsbericht 2007,3 (DE-604)BV011758990 2007,3 HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016028880&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Soda, Ante Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications Tragflügelumströmung (DE-588)4185837-2 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Transsonische Strömung (DE-588)4135633-0 gnd Grenzschichtablösung (DE-588)4136915-4 gnd |
| subject_GND | (DE-588)4185837-2 (DE-588)4690080-9 (DE-588)4135633-0 (DE-588)4136915-4 (DE-588)4113937-9 |
| title | Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications |
| title_auth | Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications |
| title_exact_search | Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications |
| title_exact_search_txtP | Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications |
| title_full | Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications Ante Soda |
| title_fullStr | Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications Ante Soda |
| title_full_unstemmed | Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications Ante Soda |
| title_short | Numerical investigation of unsteady transonic shock/boundary-layer interaction for aeronautical applications |
| title_sort | numerical investigation of unsteady transonic shock boundary layer interaction for aeronautical applications |
| topic | Tragflügelumströmung (DE-588)4185837-2 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Transsonische Strömung (DE-588)4135633-0 gnd Grenzschichtablösung (DE-588)4136915-4 gnd |
| topic_facet | Tragflügelumströmung Numerische Strömungssimulation Transsonische Strömung Grenzschichtablösung Hochschulschrift |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016028880&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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