Details
| Original language | English |
|---|---|
| Title of host publication | 43rd Fluid Dynamics Conference |
| Publication status | Published - 13 Jun 2013 |
| Event | 43rd AIAA Fluid Dynamics Conference - San Diego, CA, United States Duration: 24 Jun 2013 → 27 Jun 2013 |
Publication series
| Name | 43rd Fluid Dynamics Conference |
|---|
Abstract
Simulation capabilities for low-speed aircraft stall prediction are important for determining the limits of safe aircraft operations during design processes. The simulations are extremely demanding in terms of physical models involved, overall computation effort, and the needed efforts for validation. The present paper describes coordinated, fundamental research into new simulation methodologies for wing stall that also include the effects of atmospheric gusts. The research is carried out by the DFG funded Research Unit FOR 1066 composed of German Universities and the German Aerospace Center, DLR. The research Unit investigates advanced models of turbulence, advanced physics-based gust models, and new numerical approaches for gust simulation. These modeling and computational activities are supplemented by an unique validation experiment, that aims at providing stall data on a high-lift wing with well defined, generic distortions of the onset flow.
ASJC Scopus subject areas
- Chemical Engineering(all)
- Fluid Flow and Transfer Processes
- Energy(all)
- Energy Engineering and Power Technology
- Engineering(all)
- Aerospace Engineering
- Engineering(all)
- Mechanical Engineering
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43rd Fluid Dynamics Conference. 2013. (43rd Fluid Dynamics Conference).
Research output: Chapter in book/report/conference proceeding › Conference contribution › Research › peer review
}
TY - GEN
T1 - Simulation of Wing Stall
AU - Radespiel, Rolf
AU - François, Daniela Gisele
AU - Hoppmann, David
AU - Klein, Simon
AU - Scholz, Peter
AU - Wawrzinek, Katharina
AU - Lutz, Thorsten
AU - Auerswald, Torsten
AU - Bange, Jens
AU - Knigge, Christoph
AU - Raasch, Siegfried
AU - Kelleners, Philip
AU - Heinrich, Ralf
AU - Reuß, Silvia
AU - Probst, Axel
AU - Knopp, Tobias
N1 - Funding information: The authors gratefully acknowledge the funding of Research Unit 1066 by the Deutsche Forschungsgemeinschaft, DFG.
PY - 2013/6/13
Y1 - 2013/6/13
N2 - Simulation capabilities for low-speed aircraft stall prediction are important for determining the limits of safe aircraft operations during design processes. The simulations are extremely demanding in terms of physical models involved, overall computation effort, and the needed efforts for validation. The present paper describes coordinated, fundamental research into new simulation methodologies for wing stall that also include the effects of atmospheric gusts. The research is carried out by the DFG funded Research Unit FOR 1066 composed of German Universities and the German Aerospace Center, DLR. The research Unit investigates advanced models of turbulence, advanced physics-based gust models, and new numerical approaches for gust simulation. These modeling and computational activities are supplemented by an unique validation experiment, that aims at providing stall data on a high-lift wing with well defined, generic distortions of the onset flow.
AB - Simulation capabilities for low-speed aircraft stall prediction are important for determining the limits of safe aircraft operations during design processes. The simulations are extremely demanding in terms of physical models involved, overall computation effort, and the needed efforts for validation. The present paper describes coordinated, fundamental research into new simulation methodologies for wing stall that also include the effects of atmospheric gusts. The research is carried out by the DFG funded Research Unit FOR 1066 composed of German Universities and the German Aerospace Center, DLR. The research Unit investigates advanced models of turbulence, advanced physics-based gust models, and new numerical approaches for gust simulation. These modeling and computational activities are supplemented by an unique validation experiment, that aims at providing stall data on a high-lift wing with well defined, generic distortions of the onset flow.
UR - http://www.scopus.com/inward/record.url?scp=84883591109&partnerID=8YFLogxK
U2 - 10.2514/6.2013-3175
DO - 10.2514/6.2013-3175
M3 - Conference contribution
AN - SCOPUS:84883591109
SN - 9781624102141
T3 - 43rd Fluid Dynamics Conference
BT - 43rd Fluid Dynamics Conference
T2 - 43rd AIAA Fluid Dynamics Conference
Y2 - 24 June 2013 through 27 June 2013
ER -