Methodology for residual strength of dynamically loaded composites
Gädke, M. (2000) Methodology for residual strength of dynamically loaded composites. 20th Anniversary of DLR - CAE Cooperation, Workshop on Aeronautical Sciences & Technologies, Berlin, June 13-14,2000.
Full text not available from this repository.
In cooperation with the Aircraft Strength Research Institute of the Chinese Aeronautical Establishment (CAE) an analytical approach for modelling and calculation of the residual, strength of composites was developed during the past years in the Institute of Structural Mechanics. The main features of the approach are 1) an independent damage characterization method; 2) a new failure criterion for delamination damage; 3) a simple model for the prediction of impact damage, based on the bending strain energy density; and 4) an algorithm for the residual strength analysis of single and/or multiple delaminations, either introduced by impact or pre-implanted. The approach led to the development of a Windows compatible computer program, called "Composite Damage Tolerance Analysis Code (CDTAC)", which enables the calculation of the impact transient response, the impact damage and consequently the residual compressive strength of composite laminates, and, in an extended version, of stringer-stiffened composite panels. The comparison between calculated and experimentally evaluated impact damage zones as well as of the residual compressive strengths showed a good agreement of the results. In future work the extension of the program to the damage growth simulation under fatigue loading and the prediction of the residual strength after fatigue will be performed.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Methodology for residual strength of dynamically loaded composites|
|Event Title:||20th Anniversary of DLR - CAE Cooperation, Workshop on Aeronautical Sciences & Technologies, Berlin, June 13-14,2000|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L - no assignement|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ST - Starrflüglertechnologien|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Composite Structures and Adaptive Systems > Institut für Strukturmechanik|
|Deposited By:||Sibylle Wolff|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 16:00|
Repository Staff Only: item control page