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Vicroy, Dan D. and Huber, Kerstin Claudie and Rein, Martin and Irving, Jonathan and Rigby, Glyn and Loeser, Thomas and Birch, Trevor J. (2016) Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls. Journal of Aircraft, 55 (2), pp. 475-501. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C033782. ISSN 0021-8669.
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Official URL: http://dx.doi.org/10.2514/1.C033782
Abstract
Several static and dynamic forced-motion wind-tunnel tests on a generic unmanned combat air vehicle configuration with a 53 deg swept leading edge are reviewed. The static tests include both subsonic and transonic measurements. These tests are part of an international research effort to assess and advance the state-of-the-art of computational-fluid-dynamics methods to predict the static and dynamic stability and control characteristics for this type of configuration. The tests included analysis of trailing-edge control surface effectiveness. This paper describes the data collected from three different models of this unmanned combat air vehicle configuration in four different wind tunnels. A subset of this large experimental dataset was selected as focus test cases for computational-fluid-dynamics comparison. The focus test case data are presented in detail.
| Item URL in elib: | https://elib.dlr.de/105790/ | ||||||||||||||||||||||||||||||||
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| Document Type: | Article | ||||||||||||||||||||||||||||||||
| Title: | Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls | ||||||||||||||||||||||||||||||||
| Authors: |
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| Date: | 6 June 2016 | ||||||||||||||||||||||||||||||||
| Journal or Publication Title: | Journal of Aircraft | ||||||||||||||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||||||||||||||||||
| Volume: | 55 | ||||||||||||||||||||||||||||||||
| DOI: | 10.2514/1.C033782 | ||||||||||||||||||||||||||||||||
| Page Range: | pp. 475-501 | ||||||||||||||||||||||||||||||||
| Editors: |
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| Publisher: | American Institute of Aeronautics and Astronautics (AIAA) | ||||||||||||||||||||||||||||||||
| ISSN: | 0021-8669 | ||||||||||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||||||||||
| Keywords: | UCAV, wind tunnel testing, NaSA, DLR, BAE Systems, dstl, control surface effectiveness, subsonic and transonic measurements | ||||||||||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||||||||||||||
| HGF - Program Themes: | fixed-wing aircraft | ||||||||||||||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||||||||||||||||||||||
| DLR - Research theme (Project): | L - Military Technologies (old) | ||||||||||||||||||||||||||||||||
| Location: | Braunschweig , Göttingen | ||||||||||||||||||||||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Transport Aircraft Institute of Aerodynamics and Flow Technology > High Speed Configurations | ||||||||||||||||||||||||||||||||
| Deposited By: | Schütte, Andreas | ||||||||||||||||||||||||||||||||
| Deposited On: | 22 Aug 2016 09:22 | ||||||||||||||||||||||||||||||||
| Last Modified: | 05 Nov 2020 21:56 |
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- Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls. (deposited 22 Aug 2016 09:22) [Currently Displayed]
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