@inproceedings{HendlerExtraLockanetal., author = {Hendler, Marco and Extra, Simon and Lockan, Michael and Bestle, Dieter and Flassig, Peter Michael}, title = {Compressor Design in the Context of Holistic Aero Engine Design}, series = {2017 AIAA Aviation Forum, Denver, AIAA-2017-3334, 2017}, booktitle = {2017 AIAA Aviation Forum, Denver, AIAA-2017-3334, 2017}, doi = {10.2514/6.2017-3334}, language = {en} } @inproceedings{LockanBestleJankeetal., author = {Lockan, Michael and Bestle, Dieter and Janke, Christian and Meyer, Marcus}, title = {Optimization of Coupled System Components Using Approximations of Interface Quantities}, series = {ASME Turbo Expo 2017, Turbomachinery Conference and Exposition, Volume 2C, Turbomachinery Charlotte, North Carolina, USA, June 26-30, 2017}, booktitle = {ASME Turbo Expo 2017, Turbomachinery Conference and Exposition, Volume 2C, Turbomachinery Charlotte, North Carolina, USA, June 26-30, 2017}, publisher = {ASME}, address = {New York, NY}, isbn = {978-0-7918-5080-0}, doi = {10.1115/GT2017-64135}, pages = {11}, language = {en} } @misc{MartinBestle, author = {Martin, Ivo and Bestle, Dieter}, title = {Automated eigenmode classification for airfoils in the presence of fixation uncertainties}, series = {Engineering Applications of Artificial Intelligence}, volume = {67}, journal = {Engineering Applications of Artificial Intelligence}, issn = {0952-1976}, doi = {https://doi.org/10.1016/j.engappai.2017.09.022}, pages = {187 -- 196}, abstract = {Abstract Automated structural design optimization should take into acc ount risk of failure which depends on eigenmodes, since eigenmode shap es determine failure risk by their characteristic stress concentration pattern, as well as by their specific interaction with excitations. T hus, such a process needs to be able to identify eigenmodes with low e rror rate. This is a rather challenging task, because eigenmodes depen d on the geometry of the structure which is changing during the design process, and on boundary conditions which are not clearly defined due to uncertainties in the assembly and running conditions. The present investigation aims to find a proper classification method for eigenmod es of compressor airfoils. Specific data normalization and data depend ent initialization of a neural network using principle-component direc tions as initial weight vectors have led to the development of a class ification and decision procedure enabling automatic assignment of prop er uncertainty bands to eigenfrequencies of a specific eigenmode shape . Application to compressor airfoils of a stationary gas-turbine with hammer-foot and dove-tail roots demonstrates the high performance of t he proposed procedure.}, language = {en} } @misc{HendlerBestleFlassig, author = {Hendler, Marco and Bestle, Dieter and Flassig, Peter Michael}, title = {Component-specific Engine Design Taking into Account Holistic Design Aspects}, series = {International Journal of Turbomachinery, Propulsion and Power}, volume = {3}, journal = {International Journal of Turbomachinery, Propulsion and Power}, number = {2}, issn = {2504-186X}, doi = {10.3390/ijtpp3020012}, pages = {1 -- 16}, language = {en} } @misc{IvanovBestleJanke, author = {Ivanov, Dmitrij and Bestle, Dieter and Janke, Christian}, title = {A Response Surface Based Strategy for Accelerated Compressor Map Computation}, series = {Evolutionary and deterministic methods for design optimization and control with applications to industrial and societal problems, Sep. 13-15, 2017 in Madrid, Spain, EUROGEN 2017, Book of abstracts}, journal = {Evolutionary and deterministic methods for design optimization and control with applications to industrial and societal problems, Sep. 13-15, 2017 in Madrid, Spain, EUROGEN 2017, Book of abstracts}, publisher = {Technical University}, address = {Madrid}, isbn = {978-84-697-5112-1}, language = {en} } @misc{ExtraHendlerBestleetal., author = {Extra, Simon and Hendler, Marco and Bestle, Dieter and Flassig, Peter Michael}, title = {Verbesserte Vorauslegung des Kerntriebwerks mithilfe eines kaskadierten Optimierungsprozesses}, series = {Luft- und Raumfahrt - Digitalisierung und Vernetzung, Deutscher Luft- und Raumfahrtkongress 2018, 04.-06. September 2018, Friedrichshafen, Graf-Zeppelin-Haus}, journal = {Luft- und Raumfahrt - Digitalisierung und Vernetzung, Deutscher Luft- und Raumfahrtkongress 2018, 04.-06. September 2018, Friedrichshafen, Graf-Zeppelin-Haus}, publisher = {Deutsche Gesellschaft f{\"u}r Luft- und Raumfahrt - Lilienthal-Oberth e.V.}, address = {Bonn}, doi = {10.25967/480163}, url = {http://nbn-resolving.de/urn:nbn:de:101:1-2020011711475557798029}, pages = {10}, language = {de} } @misc{KuslitsBestle, author = {Kuslits, M{\´a}rton and Bestle, Dieter}, title = {Control Design and Performance Evaluation of a New Steering Concept Based on a Custom Multibody Vehicle Model}, series = {5th Internationa Conference on Dynamic Simulation in Vehicle Engineering}, journal = {5th Internationa Conference on Dynamic Simulation in Vehicle Engineering}, address = {Steyr}, pages = {19 -- 34}, language = {en} } @misc{KuslitsBestle, author = {Kuslits, M{\´a}rton and Bestle, Dieter}, title = {Multiobjective Performance Optimisation of a New Differential Steering Concept}, series = {Vehicle System Daynamics}, journal = {Vehicle System Daynamics}, issn = {0042-3114}, doi = {10.1080/00423114.2020.1804598}, pages = {23}, language = {en} } @inproceedings{XueSunBestleetal., author = {Xue, Rui and Sun, Lu and Bestle, Dieter and Wang, Guoping and Chen, Dongyang and Rui, Xiaoting}, title = {Vortex-induced Vibration Analysis of a composite Riser System Based on the Transfer Matrix Method}, series = {14th International Conference on Multibody Systems, Nonlinear Dynamics, and Control - Quebec City, Quebec, Canada, August 26-29, 2018}, booktitle = {14th International Conference on Multibody Systems, Nonlinear Dynamics, and Control - Quebec City, Quebec, Canada, August 26-29, 2018}, publisher = {ASME}, address = {New York}, isbn = {978-0-7918-5183-8}, pages = {10}, language = {en} } @inproceedings{SunXueBestleetal., author = {Sun, Lu and Xue, Rui and Bestle, Dieter and Wang, Guoping and Zhang, Jianshu and Rui, Xiaoting}, title = {Vibration Analysis of Linear Beam with Moving Loads Based on Riccati Transfer Matrix Method for Multibody Systems}, series = {14th International Conference on Multibody Systems, Nonlinear Dynamics, and Control - Quebec City, Quebec, Canada, August 26-29, 2018}, booktitle = {14th International Conference on Multibody Systems, Nonlinear Dynamics, and Control - Quebec City, Quebec, Canada, August 26-29, 2018}, publisher = {ASME}, address = {New York}, isbn = {978-0-7918-5183-8}, pages = {10}, language = {en} }