A study on the robustness of two stiffened composite fuselage panels
Lee, M.C.W. and Kelly, D.W. and Degenhardt, Richard and Thomson, R. (2010) A study on the robustness of two stiffened composite fuselage panels. Composite Structures, 92 (2), pp. 223-232. Elsevier Ltd.. DOI: 10.1016/j.compstruct.2009.07.009. ISSN 0263-8223.
Full text not available from this repository.
The European Commission project COCOMAT aimed at exploiting the large reserve of strength in composite structures through more accurate prediction of collapse. As part of the research program, curved stiffened composite panels of various designs have been manufactured and tested in compression. In the current pool of experiments it is possible to observe the scatter in results caused by manufacturing defects and material variations. In a bid to account for the scatter in design, two qualitative measures of robustness, called Robust Indices, have been derived so that effective comparisons can be made. The first measure quantifies robustness of structures with respect to their input variables while the second measure quantifies the overall robustness of a structure.
|Title:||A study on the robustness of two stiffened composite fuselage panels|
|Journal or Publication Title:||Composite Structures|
|In Open Access:||No|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 223-232|
|Keywords:||B. Defects; C. Statistical properties/methods; D. Mechanical testing; Robust Design|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L AR - Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Structures & Materials|
|Institutes and Institutions:||Institute of Composite Structures and Adaptive Systems > Structural Mechanics|
|Deposited By:||Doris Ries|
|Deposited On:||16 Feb 2010 11:32|
|Last Modified:||07 Feb 2013 21:05|
Repository Staff Only: item control page