Bach, Tobias (2016) NUMERICAL ASSESSMENT OF DAMAGE TOLERANCE ALLOWABLES FOR NEW DESIGN CONCEPTS OF STIFFENED COMPOSITE PANELS. 30th Congress of the International Council of the Aeronatical Sciences, 2016-09-25 - 2016-09-30, Daejeon, Korea.
|
PDF
- Only accessible within DLR
865kB |
Abstract
Within an automated framework, a structural design process is built that increases the number of design concepts applicable during the optimization of composite wings. Because Damage Tolerance allowables are determined by expensive tests for each structural concept, only one concept is usually available for the optimization. To overcome this problem, a procedure based on detailed Finite Element models has been developed, where the design concepts are modelled as super-stringers. Strain fields are evaluated to assess the capability of structural concepts the bear higher strains at a steady load level. The process is demonstrated on an I-stiffened panel with a wide range of material combinations.
| Item URL in elib: | https://elib.dlr.de/106955/ | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| Document Type: | Conference or Workshop Item (Speech) | ||||||||
| Title: | NUMERICAL ASSESSMENT OF DAMAGE TOLERANCE ALLOWABLES FOR NEW DESIGN CONCEPTS OF STIFFENED COMPOSITE PANELS | ||||||||
| Authors: |
| ||||||||
| Date: | 28 September 2016 | ||||||||
| Refereed publication: | Yes | ||||||||
| Open Access: | No | ||||||||
| Gold Open Access: | No | ||||||||
| In SCOPUS: | No | ||||||||
| In ISI Web of Science: | No | ||||||||
| Status: | Published | ||||||||
| Keywords: | Composite Panels, Design Concept, Composite Structural Optimization | ||||||||
| Event Title: | 30th Congress of the International Council of the Aeronatical Sciences | ||||||||
| Event Location: | Daejeon, Korea | ||||||||
| Event Type: | international Conference | ||||||||
| Event Start Date: | 25 September 2016 | ||||||||
| Event End Date: | 30 September 2016 | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||
| HGF - Program: | Aeronautics | ||||||||
| HGF - Program Themes: | fixed-wing aircraft | ||||||||
| DLR - Research area: | Aeronautics | ||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||
| DLR - Research theme (Project): | L - Structures and Materials (old), L - Simulation and Validation (old) | ||||||||
| Location: | Braunschweig | ||||||||
| Institutes and Institutions: | Institute of Composite Structures and Adaptive Systems > Functional Lightweight Structures | ||||||||
| Deposited By: | Bach, Tobias | ||||||||
| Deposited On: | 21 Oct 2016 16:07 | ||||||||
| Last Modified: | 24 Apr 2024 20:11 |
Repository Staff Only: item control page