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Huber, Kerstin Claudie and Schütte, Andreas and Vicroy, Dan D. and Hübner, Andreas-René (2016) UCAV MODEL DESIGN AND STATIC EXPERIMENTAL INVESTIGATIONS TO ESTIMATE CONTROL DEVICE EFFECTIVENESS AND STABILITY AND CONTROL CAPABILITIES. NATO STO - Science and Technology Organisation. [Other]
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Official URL: https://www.sto.nato.int/publications/STO%20Technical%20Reports/STO-TR-AVT-201/$$TR-AVT-201-ALL.pdf
Abstract
The experimental investigations of two generic UCAV configurations with control surfaces are presented. The current chapter is covering the design of the model, layout of the control surfaces as well as the static wind tunnel tests. The low-speed static wind tunnel tests have been undertaken to evaluate the effectiveness of different control surfaces and control surface settings. Finally, the experimental results are used to establish a common CFD test matrix for the NATO STO Task Group AVT-201 for computer code validation and to assess the capability to predict the complex vortical flow and aerodynamic Stability and Control (S&C) characteristics of configurations with highly swept leading edges and vortex-dominated flowfield.
| Item URL in elib: | https://elib.dlr.de/110903/ | ||||||||||||||||||||
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| Document Type: | Other | ||||||||||||||||||||
| Title: | UCAV MODEL DESIGN AND STATIC EXPERIMENTAL INVESTIGATIONS TO ESTIMATE CONTROL DEVICE EFFECTIVENESS AND STABILITY AND CONTROL CAPABILITIES | ||||||||||||||||||||
| Authors: |
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| Date: | 15 November 2016 | ||||||||||||||||||||
| Journal or Publication Title: | NATO STO Technical Report, RTO-AVT-TR-201 on "Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles" | ||||||||||||||||||||
| Refereed publication: | No | ||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||
| DOI: | 10.14339/STO-TR-AVT-201 | ||||||||||||||||||||
| Number of Pages: | 22 | ||||||||||||||||||||
| Publisher: | NATO STO - Science and Technology Organisation | ||||||||||||||||||||
| ISBN: | 978-92-837-2079-9 | ||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||
| Keywords: | UCAV, Delta wing, vortical flow, stability and control, control surfaces, SACCON, AVT-201, validation, experiment, NATO, AVT, STO, prediction methods, maneuver simulation | ||||||||||||||||||||
| 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 German-Dutch Windtunnels | ||||||||||||||||||||
| Deposited By: | Schütte, Andreas | ||||||||||||||||||||
| Deposited On: | 02 Feb 2017 09:48 | ||||||||||||||||||||
| Last Modified: | 02 Feb 2017 15:56 |
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