Stradtner, Mario and Drazen, David A. and van Rooij, Michel P.C. (2024) Enhanced Computational Performance and Stability & Control Prediction for NATO Military Vehicles. In: AIAA Aviation Forum and ASCEND, 2024. American Institute of Aeronautics and Astronautics, Inc. AIAA AVIATION FORUM AND ASCEND 2024, 2024-07-29 - 2024-08-02, Las Vegas, NV, USA. doi: 10.2514/6.2024-4064. ISBN 978-162410-716-0.
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Official URL: https://arc.aiaa.org/doi/10.2514/6.2024-4064
Abstract
The NATO Science & Technology Organisation Research Task Group Applied Vehicle Technology (AVT)-351 of the Applied Vehicle Technology panel worked on the development of enhanced numerical methods to efficiently generate comprehensive performance, stability and control data sets at feasible cost for air and sea vehicles based on computational fluid dynamic and experiment data. Currently the use of computational fluid dynamics and experiments for military vehicle design is limited by the tremendous cost and timescales necessary for providing comprehensive data sets. A feasible means to overcome these limitations are reduced-order modeling techniques by making efficient use of a limited amount of highly accurate experimental and computational data points. Reduced-order models that are capable of time-dependent maneuver prediction and data set population are investigated and applied on four different air and sea vehicle use cases. This paper presents a summary of the research task group, use cases, methods and results of various reduced-order models and provides an extension to a previously published introduction to this research task group.
| Item URL in elib: | https://elib.dlr.de/208974/ | ||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||
| Title: | Enhanced Computational Performance and Stability & Control Prediction for NATO Military Vehicles | ||||||||||||||||
| Authors: |
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| Date: | 29 July 2024 | ||||||||||||||||
| Journal or Publication Title: | AIAA Aviation Forum and ASCEND, 2024 | ||||||||||||||||
| Refereed publication: | No | ||||||||||||||||
| Open Access: | No | ||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||
| DOI: | 10.2514/6.2024-4064 | ||||||||||||||||
| Publisher: | American Institute of Aeronautics and Astronautics, Inc | ||||||||||||||||
| ISBN: | 978-162410-716-0 | ||||||||||||||||
| Status: | Published | ||||||||||||||||
| Keywords: | Model Order Reduction, Aerodynamic Performance, Aerodynamic Characteristics, Computational Fluid Dynamics | ||||||||||||||||
| Event Title: | AIAA AVIATION FORUM AND ASCEND 2024 | ||||||||||||||||
| Event Location: | Las Vegas, NV, USA | ||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||
| Event Start Date: | 29 July 2024 | ||||||||||||||||
| Event End Date: | 2 August 2024 | ||||||||||||||||
| Organizer: | American Institute of Aeronautics and Astronautics, Inc. | ||||||||||||||||
| HGF - Research field: | other | ||||||||||||||||
| HGF - Program: | other | ||||||||||||||||
| HGF - Program Themes: | other | ||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||
| DLR - Program: | L DT - Defense Technology | ||||||||||||||||
| DLR - Research theme (Project): | L - Effect | ||||||||||||||||
| Location: | Braunschweig | ||||||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > CASE, BS | ||||||||||||||||
| Deposited By: | Stradtner, Mario | ||||||||||||||||
| Deposited On: | 04 Dec 2024 11:02 | ||||||||||||||||
| Last Modified: | 04 Dec 2024 11:02 |
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