Crash and High Velocity Impact Simulation Methodologies for Aircraft Structures
Kindervater, C.M and Johnson, A, and Kohlgrüber, D, and Lützenburger, M. (2000) Crash and High Velocity Impact Simulation Methodologies for Aircraft Structures. Structural Failure and Plasticity (IMPLAST 2000), IMPLAST 2000, .
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Numerical crash and high velocity simulation studies of metallic and composite sub-components of aircraft structures are presented which were performed within various European Commission (CEC) sponsored research projects. Both hybrid simulation techniques as well as Finite Element (FE) based crash codes were used. Several new composite material models were developed and validated against tests. Especially with the metallic structures, the simulations correlated well with data of impact tests which were performed within the programs.
|Title:||Crash and High Velocity Impact Simulation Methodologies for Aircraft Structures|
|Journal or Publication Title:||Structural Failure and Plasticity (IMPLAST 2000)|
|In ISI Web of Science:||No|
|Keywords:||crash, simulation, finite element, numerical analysis, aircraft|
|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 Structures and Design|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 22:19|
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