Kensche, C. and Krause, O. (2003) Lifetime prediction of highly loaded composite structures. 18th Annual Technical Conference, Gainesville, Florida, 20-22 Oktober 2003.
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A method of lifetime approval for composite spar beams has been developed. At first, the general fatigue response of the used material components has to be evaluated. Using a FE-analysis, the critical areas of the structure are identified and the design stresses evaluated. Subsequently, a lifetime prediction with a Miners damage summation rule of the most fatigue sensitive part of the structure is done. Incorporating the correlation of variable and constant amplitude loading, the predicted lifetime may be verified with time-saving proof tests.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Lifetime prediction of highly loaded composite structures|
|Keywords:||fatigue, lifetime prediction, proof test|
|Event Title:||18th Annual Technical Conference, Gainesville, Florida, 20-22 Oktober 2003|
|Organizer:||American Society of Composites|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Structures and Design|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 13:15|
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