A simulation environment is presented for special structural dynamics investigations. The environment is characterised by a modular software structure and an object-oriented data-structure. The aircraft model and equation of motion can easily be adapted to the required level of detail. An integrated, fully flexible aircraft model is the basis for the simulations. The novelty of the approach lies in the combination of the above mentioned characteristics. It is demonstrated that this combination makes the software environment ideally suited for special studies ranging from the preliminary design stage on to in-flight incident investigations.
A Variable, Fully Flexible Dynamic Response Tool for Special Investigations (VarLoads)
2003 ; Amsterdam
2003
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2004
|SAE Technical Papers | 2005
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