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Löser, Thomas and Vicroy, Dan D. and Schütte, Andreas (2009) SACCON STATIC WIND TUNNEL TESTS AT DNW-NWB AND 14ft × 22ft NASA LARC. NATO RTO - Research and Technology Organisation. [Other]
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Official URL: https://www.sto.nato.int/publications/STO%20Technical%20Reports/RTO-TR-AVT-161/$$TR-AVT-161-ALL.pdf
Abstract
Static force and pressure measurement results obtained from three test campaigns in two different wind tunnels are presented. The model investigated was the generic UCAF configuration SACCON. Model design, manufacture, as well as three wind tunnel entries have been performed within the NATO/RTO AVT-161 Task Group “Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles”. The model has undergone static as well as dynamic tests as an international co-operation; the tests have been accompanied by corresponding numerical investigations. This chapter covers the static part of the wind tunnel experiments. Model and instrumentation are described in detail and, focussing on the force measurement results, the effects of the different parameters are explained.
| Item URL in elib: | https://elib.dlr.de/110896/ | ||||||||||||||||
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| Document Type: | Other | ||||||||||||||||
| Title: | SACCON STATIC WIND TUNNEL TESTS AT DNW-NWB AND 14ft × 22ft NASA LARC | ||||||||||||||||
| Authors: |
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| Date: | 4 September 2009 | ||||||||||||||||
| Journal or Publication Title: | NATO RTO Technical Report, RTO-AVT-TR-161 on "Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles" | ||||||||||||||||
| Refereed publication: | No | ||||||||||||||||
| Open Access: | No | ||||||||||||||||
| DOI: | 10.14339/RTO-TR-AVT-161 | ||||||||||||||||
| Number of Pages: | 22 | ||||||||||||||||
| Publisher: | NATO RTO - Research and Technology Organisation | ||||||||||||||||
| Status: | Published | ||||||||||||||||
| Keywords: | UCAV, Delta wing, vortical flow, stability and control, validation, Experiment, NATO, AVT, RTO, DNW-NWB, MPM, NASA. dynamic tests, maneuver | ||||||||||||||||
| 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 | ||||||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology German-Dutch Windtunnels | ||||||||||||||||
| Deposited By: | Schütte, Andreas | ||||||||||||||||
| Deposited On: | 30 Jan 2017 10:05 | ||||||||||||||||
| Last Modified: | 30 Jan 2017 10:05 |
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