Contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures:
Gespeichert in:
1. Verfasser: | |
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Format: | Abschlussarbeit Buch |
Sprache: | English |
Veröffentlicht: |
Aachen
Shaker
2007
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Schriftenreihe: | Berichte aus der Luft- und Raumfahrttechnik
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Schlagworte: | |
Online-Zugang: | Inhaltsverzeichnis |
Beschreibung: | 199 S. Ill., graph. Darst. |
ISBN: | 383226809X |
Internformat
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Datensatz im Suchindex
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adam_text | CONTRIBUTION TO THE UNDER- STANDING AND IMPROVEMENT OF FATIGUE CRACK
GROWTH BEHAVIOUR OF BONDED AIRCRAFT STRUCTURES VON DER FAKULTAT FUR
LUFT- UND RAUMFAHRTTECHNIK UND GEODASIE DER UNIVERSITAT STUTTGART ZUR
ERIANGUNG DER WIIRDE EINES DOKTOR-LNGENIEURS (DR.-ING.) GENEHMIGTE
ABHANDLUNG VORGELEGT VON BERNHARD KURZ AUS ALTOTTING HAUPTBERICHTER:
PROF. DR.-LNG. K. DRECHSLER MITBERICHTER: PROF. DR.-LNG. L. LAZZERI
PROF. DR.-LNG. H. VOGGENREITER TAG DER MUNDLICHEN PRUFUNG: 22. OKTOBER
2007 INSTITUT FUR FLUGZEUGBAU DER UNIVERSITAT STUTTGART 2007
ZUSAMMENFASSUNG 9 ABSTRACT 11 1 HISTORY OF BONDING IN AIRFRAME
MANUFACTURING 13 2 BASICS AND STATE OF THE ART 15 2.1 FRACTURE MECHANICS
15 2.1.1 LINEAR ELASTIC FRACTURE MECHANICS 16 2.1.2 FATIGUE CRACK
PROPAGATION 22 2.1.3 ELASTIC PLASTIC FRACTURE MECHANICS 28 2.2 BONDING
35 2.2.1 ADVANTAGES OF BONDED STRUCTURES 38 2.2.2 STRUCTURAL ADHESIVE
JOINT CONFIGURATIONS 47 2.2.3 BONDED SINGLE LAP JOINT 48 2.3 FEA -
FINITE ELEMENT ANALYSIS 52 2.3.1 FE-THEORY 53 2.3.2 H- AND P-ELEMENTS :
54 2.3.3 MATERIAL MODELS 57 2.3.4 CALCULATION OF STRAIN ENERGY RELEASE
RATE 62 2.3.5 SUMMARY 64 3 EXPERIMENTS 65 3.1 DETERMINATION OF THE
ADHESIVE PROPERTIES 69 3.2 FATIGUE CRACK GROWTH TESTS 73 3.3 SPECIMEN
WITH TWO DOUBLERS 75 3.4 SPECIMEN WITH TWO STRINGERS 79 3.5 7-STRINGER
SPECIMEN 81 3.6 CUT OUT OF 7-STRINGER SPECIMEN 88 4 FE-SIMULATION . 93
4.1 SINGLE LAP JOINT 93 4.1.1 STRESSCHECK 94 RECKKIGCHE UNIVERSITAT
DARMSTADT FOCHPEBLCT KONSTRUKTLVER LEICHTBAU UND BSUWCLSEN PROF.
DR.-LNG. HELMUT SCHQRMANN *54287 DARMSTADT, PETERSENSTRARE 30 4.1.2
ANSYS 98 4.2 INVESTIGATION ON THE RADIUS OF INTEGRATION 104 4.3
INFLUENCE OF THE ANTI BUCKLING DEVICE 109 4.4 COMPARISON OF A MONOLITHIC
AND A METAL LAMINATE SKIN 112 4.5 M(T)-SPECIMEN 113 4.5.1 MONOLITHIC
M(T) SPECIMEN 114 4.5.2 METAL LAMINATE M(T) SPECIMEN 120 4.6 SPECIMEN
WITH TWO DOUBLERS . 123 4.6.1 COMPARISON OF EXPERIMENTAL TESTS AND FE
ANALYSIS AT A SPECIMEN WITH TWO DOUBLERS 123 4.6.2 MATERIAL AND GEOMETRY
INVESTIGATION OF THE DOUBLER 127 4.6.3 PREPREG LAYER BELOW THE DOUBLER
136 4.7 SPECIMEN WITH TWO STRINGERS 140 4.7.1 INFLUENCE OF THE STRINGER
GEOMETRY 140 4.7.2 NEW DESIGN OF STRINGER GEOMETRIES 142 4.8 7-STRINGER
PANEL 150 4.8.1 MODEL CREATION 150 4.8.2 STATIC PRE-LOAD 150 4.8.3
FATIGUE CRACK GROWTH SIMULATION 152 4.8.4 DEBONDING OF THE STRINGER 154
4.8.5 ANALYSIS OF THE STRINGER FAILURE 156 4.9 CUT OUT OF 7-STRINGER
SPECIMEN 163 5 DISCUSSION AND SUMMARY 169 6 LITERATURE 175 7 APPENDIX
187 7.1 LIST OF FIGURES 187 7.2 LIST OF TABLES 194 8 CURRICULUM VITAE
197 9 ACKNOWLEDGEMENT 199
|
any_adam_object | 1 |
author | Kurz, Bernhard |
author_facet | Kurz, Bernhard |
author_role | aut |
author_sort | Kurz, Bernhard |
author_variant | b k bk |
building | Verbundindex |
bvnumber | BV023803677 |
classification_rvk | ZM 3900 |
ctrlnum | (OCoLC)244011631 (DE-599)BVBBV023803677 |
dewey-full | 629.1345 |
dewey-hundreds | 600 - Technology (Applied sciences) |
dewey-ones | 629 - Other branches of engineering |
dewey-raw | 629.1345 |
dewey-search | 629.1345 |
dewey-sort | 3629.1345 |
dewey-tens | 620 - Engineering and allied operations |
discipline | Werkstoffwissenschaften / Fertigungstechnik Verkehr / Transport |
format | Thesis Book |
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genre_facet | Hochschulschrift |
id | DE-604.BV023803677 |
illustrated | Illustrated |
indexdate | 2024-07-09T21:37:10Z |
institution | BVB |
isbn | 383226809X |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-017445875 |
oclc_num | 244011631 |
open_access_boolean | |
owner | DE-634 DE-83 |
owner_facet | DE-634 DE-83 |
physical | 199 S. Ill., graph. Darst. |
publishDate | 2007 |
publishDateSearch | 2007 |
publishDateSort | 2007 |
publisher | Shaker |
record_format | marc |
series2 | Berichte aus der Luft- und Raumfahrttechnik |
spelling | Kurz, Bernhard Verfasser aut Contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures Bernhard Kurz Aachen Shaker 2007 199 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Berichte aus der Luft- und Raumfahrttechnik Zugl.: Stuttgart, Univ., Diss., 2007 Metallklebeverbindung (DE-588)4169601-3 gnd rswk-swf Zerstörende Werkstoffprüfung (DE-588)4241901-3 gnd rswk-swf Rissausbreitung (DE-588)4136911-7 gnd rswk-swf Finite-Elemente-Methode (DE-588)4017233-8 gnd rswk-swf Flugzeug (DE-588)4017672-1 gnd rswk-swf (DE-588)4113937-9 Hochschulschrift gnd-content Metallklebeverbindung (DE-588)4169601-3 s Flugzeug (DE-588)4017672-1 s Rissausbreitung (DE-588)4136911-7 s Zerstörende Werkstoffprüfung (DE-588)4241901-3 s DE-604 Finite-Elemente-Methode (DE-588)4017233-8 s HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=017445875&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
spellingShingle | Kurz, Bernhard Contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures Metallklebeverbindung (DE-588)4169601-3 gnd Zerstörende Werkstoffprüfung (DE-588)4241901-3 gnd Rissausbreitung (DE-588)4136911-7 gnd Finite-Elemente-Methode (DE-588)4017233-8 gnd Flugzeug (DE-588)4017672-1 gnd |
subject_GND | (DE-588)4169601-3 (DE-588)4241901-3 (DE-588)4136911-7 (DE-588)4017233-8 (DE-588)4017672-1 (DE-588)4113937-9 |
title | Contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures |
title_auth | Contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures |
title_exact_search | Contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures |
title_full | Contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures Bernhard Kurz |
title_fullStr | Contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures Bernhard Kurz |
title_full_unstemmed | Contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures Bernhard Kurz |
title_short | Contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures |
title_sort | contribution to the understanding and improvement of fatigue crack growth behaviour of bonded aircraft structures |
topic | Metallklebeverbindung (DE-588)4169601-3 gnd Zerstörende Werkstoffprüfung (DE-588)4241901-3 gnd Rissausbreitung (DE-588)4136911-7 gnd Finite-Elemente-Methode (DE-588)4017233-8 gnd Flugzeug (DE-588)4017672-1 gnd |
topic_facet | Metallklebeverbindung Zerstörende Werkstoffprüfung Rissausbreitung Finite-Elemente-Methode Flugzeug Hochschulschrift |
url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=017445875&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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