This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Virtual Testing for High Lift Systems
Technical Paper
2011-01-2754
ISSN: 0148-7191, e-ISSN: 2688-3627
Annotation ability available
Sector:
Language:
English
Abstract
Improving the verification and certification process of the high lift system by introduction of virtual testing is one of the approaches to counter the challenges related to testing of future aircraft, in terms of performing more tests of more complex systems in less time. The quality of the applied modelling methods itself and the guarantee of a completely traceable simulation lifecycle management along the aircraft development are essential.
The presentation shows how existing processes for the management of all test related data have to be extended to cover the specifics of using multi body simulation models for virtual tests related to high lift failure cases. Based on a demonstrator, MSC Software GmbH and Airbus developed and are still refining the SimManager based “High Lift System Virtual Test Portal”.
This portal has to fulfil on the one side global requirements like data management, data traceability and workflow management. On the other hand, also specific requirements coming from the high lift test department have to be fulfilled. The major requirements are connection to an existing test management system (TMS), starting the execution of test procedures within MSC ADAMS, evaluation of simulation results (e.g. extraction of key results) and feedback of relevant data to the TMS.
Recent and ongoing enhancements are e.g. the possibility of execution of multiple simulation runs to create data for investigation of parameter dependencies or DOE. Furthermore the portal is enlarged by functionalities tracking besides virtual test execution also the creation process of the corresponding simulation models.
The presentation will give an overview of the virtual test integration and customization within the high lift test environment.
Recommended Content
Technical Paper | Development of the Multi-Resolution Modeling Environment through Aircraft Scenarios |
Technical Paper | Tools for Integration of Analysis and Testing |
Technical Paper | Non-Intrusive Partial Discharges Investigations on Aeronautic Motors |
Authors
Topic
Citation
Ulmer, T., "Virtual Testing for High Lift Systems," SAE Technical Paper 2011-01-2754, 2011, https://doi.org/10.4271/2011-01-2754.Also In
References
- Gülzau, H Carl, U.B. 2007 Parametric Modelling and Experimental Validation of multi body simulation of elastic flap systems in transport aircraft Estorff, O. 2007 1 st International Workshop on Aircraft System Technologies Hamburg TUHH 39 48
- MSC 2008 MSC SimManager R3.1 User's Guide MSC.Software
- VIVACE Consortium Members 2007 Final Technical Achievements System Simulation 12ff