A virtual testing approach for honeycomb sandwich panel joints in aircraft interior:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Berlin
Springer Vieweg
[2020]
|
| Schriftenreihe: | Produktentwicklung und Konstruktionstechnik
Band 16 |
| Schlagworte: | |
| Online-Zugang: | Inhaltstext http://www.springer.com/ Inhaltsverzeichnis |
| Beschreibung: | XVI, 199 Seiten Illustrationen, Diagramme |
| ISBN: | 9783662602751 366260275X |
Internformat
MARC
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| 245 | 1 | 0 | |a A virtual testing approach for honeycomb sandwich panel joints in aircraft interior |c Ralf Seemann |
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| 300 | |a XVI, 199 Seiten |b Illustrationen, Diagramme | ||
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| 653 | |a Virtual Testing | ||
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Datensatz im Suchindex
| _version_ | 1817968105462169600 |
|---|---|
| adam_text |
TABLE
OF
CONTENTS
1
INTRODUCTION
.
1
1.1
MOTIVATION
.
1
1.2
THESIS
OBJECTIVES
.
2
1.3
THESIS
STRUCTURE
.
2
2
STATE
OF
THE
ART
.
5
2.1
SANDWICH
STRUCTURES
.
5
2.1.1
FACE
SHEETS
.
5
2.1.2
CORE
.
7
2.1.3
BONDED
SANDWICH
PANEL
.
8
2.1.4
FAILURE
MODES
.
11
2.2
SANDWICH
STRUCTURE
JOINTS
.
12
2.2.1
INSERTS
.
12
2.2.2
PANEL
EDGES
.
15
2.2.3
NOVEL
JOINT
DESIGNS
.
16
2.3
COMPUTATIONAL
ANALYSIS
.
17
2.3.1
FINITE
ELEMENT
METHOD
.
19
2.3.2
LITERATURE
SURVEY
ON
SANDWICH
PANEL
JOINT
MODELLING
.
22
2.4
VIRTUAL
TESTING
.
23
2.5
ASSESSMENT
OF
THE
STATE
OF
THE
ART
AND
NEED
FOR
FURTHER
RESEARCH
.
30
3
OVERALL
CONCEPT
OF
MECHANICAL
CHARACTERIZATION
.
33
4
MECHANICAL
CHARACTERIZATION
ON
CONSTITUENT
LEVEL
.
35
4.1
SANDWICH
CORE
.
35
4.1.1
MATERIALS
.
36
4.1.2
EXPERIMENTAL
ANALYSIS
.
39
4.1.3
NUMERICAL
MODELLING
ON
MESO
SCALE
.
44
4.1.4
NUMERICAL
MODELLING
WITH
3D-CONTIUUM
ELEMENTS
.
59
4.1.5
CONCLUSION
.
62
4.2
FACE
SHEETS
.
62
4.2.1
EXPERIMENTAL
ANALYSIS
.
64
4.2.2
NUMERICAL
MODELLING
AND
CALIBRATION
.
65
4.3
ADHESIVES
.
68
4.3.1
EXPERIMENTAL
ANALYSIS
.
68
4.3.2 NUMERICAL
MODELLING
AND
CALIBRATION
.
72
5
MECHANICAL
CHARACTERIZATION
ON
STRUCTURAL
ELEMENT
LEVEL
.
73
5.1
PANEL
FLEXURE
.
73
5.1.1
EXPERIMENTAL
ANALYSIS
.
75
5.1.2
NUMERICAL
ANALYSIS
.
79
5.2
IN-PLANE
SHEAR
.
87
5.2.1
EXPERIMENTAL
ANALYSIS
.
87
5.2.2
NUMERICAL
ANALYSIS
.
88
5.3
ADDITIONAL
TEST
METHODS
.
91
6
MECHANICAL
CHARACTERIZATION
ON
SUB
COMPONENT
LEVEL
.
95
6.1
THREADED
INSERTS
PERPENDICULAR
TO
THE
FACE
SHEET
.
95
6.1.1
OUT-OF-PLANE
TENSION
(PULL-OUT)
.
96
6.1.2
IN-PLANE
TENSION
(SHEAR)
.
99
6.2
L-JOINTS.
100
6.2.1
L-JOINT
BENDING
TEST
.
101
6.2.2
L-JOINT
SHEAR
TEST
.
102
7
VIRTUAL
TESTING
APPROACH
FOR
SANDWICH
PANEL
JOINTS
.
105
7.1
OVERVIEW
.
105
7.2
PHASE
1
-
PROBLEM
ANALYSIS
.
106
7.3
PHASE
2
-
DEFINITION
OF
MODEL
FRAMEWORK
.
110
7.4
PHASE
3
-
MODEL
DEVELOPMENT
.
114
7.4.1
INVESTIGATION
.
115
7.4.2
BUILDING
BLOCKS
.
125
7.4.3
MODELLING
DATABASE
.
136
7.5
PHASE
4
-
APPLICATION
OF
VIRTUAL
TEST
.
136
7.6
SUMMARY
.
140
7.7
VALIDATION
BASED
ON
DIFFERENT
JOINT
CONFIGURATIONS
.
141
7.7.1
PARTIALLY
POTTED
INSERTS
.
141
7.7.2
CORNER
JOINTS
.
148
7.7.3
CONCLUSION
.
153
8
DEVELOPMENT
OF
NOVEL
SANDWICH
PANEL
JOINTS
.
155
8.1
VIRTUAL
TESTING
OF
DESIGN
ALTERNATIVES
.
157
8.2
VALIDATION
BY
EXPERIMENTAL
INVESTIGATION
.
160
9
SUMMARY
AND
OUTLOOK
.
163
LITERATURE
.
165
APPENDIX
A
-
CONSTITUENT
LEVEL
.
179
AL
IMPLEMENTED
MATERIAL
MODELS
OF
NOMEX
HONEYCOMB
.
179
A2
IMPLEMENTED
MATERIAL
MODELS
FOR
FACE
SHEETS
.
183
A3
IMPLEMENTED
MATERIAL
MODELS
FOR
ADHESIVES
.
187
APPENDIX
B
-
STRUCTURAL
ELEMENT
LEVEL
.
192
BL
SANDWICH
BENDING
TEST
DETAILS
.
192
B2
COMPARISON
OF
MODELLING
APPROACHES
IN
CASE
OF
BENDING
.
194
B3
FRAME
SHEAR
TEST
DETAILS
.
195
APPENDIX
C
-
SUB
COMPONENT
LEVEL.
196
CL
DAMAGE
PROGRESSION
FOR
PULL-OUT
TEST
ON
FULLY
POTTED
INSERT
.
196
C2
IMPLEMENTED
COHESIVE
BEHAVIOR
OF
POTTING-FACE
CONTACT
.
197
C3
EXPERIMENTAL
RESULTS
IN
NOVEL
DESIGN
STUDY
.
198 |
| any_adam_object | 1 |
| author | Seemann, Ralf 1985- |
| author_GND | (DE-588)1200661443 |
| author_facet | Seemann, Ralf 1985- |
| author_role | aut |
| author_sort | Seemann, Ralf 1985- |
| author_variant | r s rs |
| building | Verbundindex |
| bvnumber | BV046249712 |
| classification_rvk | ZO 7210 |
| ctrlnum | (OCoLC)1137837593 (DE-599)DNB1192030648 |
| discipline | Maschinenbau / Maschinenwesen Verkehr / Transport |
| format | Book |
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| id | DE-604.BV046249712 |
| illustrated | Illustrated |
| indexdate | 2024-12-09T13:04:48Z |
| institution | BVB |
| institution_GND | (DE-588)1065168780 |
| isbn | 9783662602751 366260275X |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-031627954 |
| oclc_num | 1137837593 |
| open_access_boolean | |
| owner | DE-83 |
| owner_facet | DE-83 |
| physical | XVI, 199 Seiten Illustrationen, Diagramme |
| publishDate | 2020 |
| publishDateSearch | 2020 |
| publishDateSort | 2020 |
| publisher | Springer Vieweg |
| record_format | marc |
| series | Produktentwicklung und Konstruktionstechnik |
| series2 | Produktentwicklung und Konstruktionstechnik |
| spelling | Seemann, Ralf 1985- Verfasser (DE-588)1200661443 aut A virtual testing approach for honeycomb sandwich panel joints in aircraft interior Ralf Seemann Berlin Springer Vieweg [2020] XVI, 199 Seiten Illustrationen, Diagramme txt rdacontent n rdamedia nc rdacarrier Produktentwicklung und Konstruktionstechnik Band 16 Testen (DE-588)4367264-4 gnd rswk-swf Faserverbundwerkstoff (DE-588)4134341-4 gnd rswk-swf Flugzeugbau (DE-588)4154782-2 gnd rswk-swf Flugzeugkabine (DE-588)4154784-6 gnd rswk-swf Fuge Bauwesen (DE-588)4018840-1 gnd rswk-swf Verbindungselement (DE-588)4062621-0 gnd rswk-swf Mechanisches Versagen (DE-588)4343948-2 gnd rswk-swf Mechanische Eigenschaft (DE-588)4217961-0 gnd rswk-swf Festigkeit (DE-588)4016916-9 gnd rswk-swf Methodenbank (DE-588)4139013-1 gnd rswk-swf Honigwabe Technik (DE-588)1152348167 gnd rswk-swf Wabenbauweise (DE-588)4139618-2 gnd rswk-swf Sandwichbauweise (DE-588)4051569-2 gnd rswk-swf Hardback TEC009070 TGB Aerospace Technology and Astronautics Finite Element Method Nomex Honeycomb Sandwich Structures Virtual Testing TEC021000 TGM C SCT17004: Mechanical Engineering SCT28000: Materials Engineering SCZ11000: Structural Materials SUCO11647: Engineering 1682: Hardcover, Softcover / Technik/Maschinenbau, Fertigungstechnik Sandwichbauweise (DE-588)4051569-2 s Honigwabe Technik (DE-588)1152348167 s Faserverbundwerkstoff (DE-588)4134341-4 s Verbindungselement (DE-588)4062621-0 s Festigkeit (DE-588)4016916-9 s Mechanisches Versagen (DE-588)4343948-2 s Mechanische Eigenschaft (DE-588)4217961-0 s Methodenbank (DE-588)4139013-1 s Testen (DE-588)4367264-4 s Flugzeugkabine (DE-588)4154784-6 s DE-604 Wabenbauweise (DE-588)4139618-2 s Flugzeugbau (DE-588)4154782-2 s Fuge Bauwesen (DE-588)4018840-1 s Springer-Verlag GmbH (DE-588)1065168780 pbl Erscheint auch als Online-Ausgabe 978-3-662-60276-8 Produktentwicklung und Konstruktionstechnik Band 16 (DE-604)BV046356265 16 X:MVB text/html http://deposit.dnb.de/cgi-bin/dokserv?id=84bb94ea9ff049e4a7fd80389c82b780&prov=M&dok_var=1&dok_ext=htm Inhaltstext X:MVB http://www.springer.com/ DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=031627954&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Seemann, Ralf 1985- A virtual testing approach for honeycomb sandwich panel joints in aircraft interior Produktentwicklung und Konstruktionstechnik Testen (DE-588)4367264-4 gnd Faserverbundwerkstoff (DE-588)4134341-4 gnd Flugzeugbau (DE-588)4154782-2 gnd Flugzeugkabine (DE-588)4154784-6 gnd Fuge Bauwesen (DE-588)4018840-1 gnd Verbindungselement (DE-588)4062621-0 gnd Mechanisches Versagen (DE-588)4343948-2 gnd Mechanische Eigenschaft (DE-588)4217961-0 gnd Festigkeit (DE-588)4016916-9 gnd Methodenbank (DE-588)4139013-1 gnd Honigwabe Technik (DE-588)1152348167 gnd Wabenbauweise (DE-588)4139618-2 gnd Sandwichbauweise (DE-588)4051569-2 gnd |
| subject_GND | (DE-588)4367264-4 (DE-588)4134341-4 (DE-588)4154782-2 (DE-588)4154784-6 (DE-588)4018840-1 (DE-588)4062621-0 (DE-588)4343948-2 (DE-588)4217961-0 (DE-588)4016916-9 (DE-588)4139013-1 (DE-588)1152348167 (DE-588)4139618-2 (DE-588)4051569-2 |
| title | A virtual testing approach for honeycomb sandwich panel joints in aircraft interior |
| title_auth | A virtual testing approach for honeycomb sandwich panel joints in aircraft interior |
| title_exact_search | A virtual testing approach for honeycomb sandwich panel joints in aircraft interior |
| title_full | A virtual testing approach for honeycomb sandwich panel joints in aircraft interior Ralf Seemann |
| title_fullStr | A virtual testing approach for honeycomb sandwich panel joints in aircraft interior Ralf Seemann |
| title_full_unstemmed | A virtual testing approach for honeycomb sandwich panel joints in aircraft interior Ralf Seemann |
| title_short | A virtual testing approach for honeycomb sandwich panel joints in aircraft interior |
| title_sort | a virtual testing approach for honeycomb sandwich panel joints in aircraft interior |
| topic | Testen (DE-588)4367264-4 gnd Faserverbundwerkstoff (DE-588)4134341-4 gnd Flugzeugbau (DE-588)4154782-2 gnd Flugzeugkabine (DE-588)4154784-6 gnd Fuge Bauwesen (DE-588)4018840-1 gnd Verbindungselement (DE-588)4062621-0 gnd Mechanisches Versagen (DE-588)4343948-2 gnd Mechanische Eigenschaft (DE-588)4217961-0 gnd Festigkeit (DE-588)4016916-9 gnd Methodenbank (DE-588)4139013-1 gnd Honigwabe Technik (DE-588)1152348167 gnd Wabenbauweise (DE-588)4139618-2 gnd Sandwichbauweise (DE-588)4051569-2 gnd |
| topic_facet | Testen Faserverbundwerkstoff Flugzeugbau Flugzeugkabine Fuge Bauwesen Verbindungselement Mechanisches Versagen Mechanische Eigenschaft Festigkeit Methodenbank Honigwabe Technik Wabenbauweise Sandwichbauweise |
| url | http://deposit.dnb.de/cgi-bin/dokserv?id=84bb94ea9ff049e4a7fd80389c82b780&prov=M&dok_var=1&dok_ext=htm http://www.springer.com/ http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=031627954&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| volume_link | (DE-604)BV046356265 |
| work_keys_str_mv | AT seemannralf avirtualtestingapproachforhoneycombsandwichpaneljointsinaircraftinterior AT springerverlaggmbh avirtualtestingapproachforhoneycombsandwichpaneljointsinaircraftinterior |