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TAU User Meeting 2011
October 18 + 19, 2011
DLR Braunschweig
The TAU User Meeting was intended to give TAU users in academia and industry the opportunity to demonstrate their applications, to share their experiences and to discuss their needs with specialists. Recent TAU developments were highlighted and future activities discussed.
The talks covered the following topics:
- fixed-wing aircraft,
- rotary-wing aircraft,
- defense applications,
- spacecraft,
- TAU Developments.
A poster session during coffee breaks was devoted to results of the MUNA national research project on uncertainties in numerical simulation.
The TAU User Meeting was concluded by a panel discussion with members of the development team.
A flyer with detailed information can be found here.
Agenda TAU User Meeting 2011
Tuesday, October 18, 2011
8:00 - 8:50 | Registration |
8:50 - 9:00 | Welcome |
9:00 - 11:30 | 1st session Chair: Norbert Kroll (DLR-AS-CA) |
9:00 - 9:30 | Recent applications of TAU at Airbus |
9:30 - 10:00 | CFD TAU cases within the aerodynamic design process |
10:00 - 10:30 | Recent investigations on the A400M with emphasis on fuselage / tails topics |
10:30 - 11:00 | Installation effects of a CROR propulsion system on a modified DLR-F6 aircraft configuration |
11:00 - 11:30 | Active separation control for high-lift configurations using a URANS approach |
11:30 - 12:30 - Lunch
12:30 - 15:00 | 2nd session Chair: Scott Shaw (Airbus) |
12:30 - 13:00 | Recent TAU applications at ARA using SOLAR meshes |
13:00 - 13:30 | FlowSimulator - A parallel environment for multidisciplinary CFD simulations |
13:30 - 14:00 | A reduced-order modeling approach for the efficient computation of high-lift aerodynamics with TAU |
14:00 - 14:30 | Unsteady TAU and ROM for flutter computations of transport aircraft |
14:30 - 15:00 | Multidisciplinary gust encounter simulation with TAU |
15:00 - 16:00 - Coffee break & poster presentations
16:00 - 18:30 | 3rd session Chair: Ralf Rudnik (DLR-AS-TF) |
16:00 - 16:30 | Experimental and numerical investigation of the flow topology during airdrop operations |
16:30 - 17:00 | Geometry parameterization for aerodynamic shape optimization in the context of highfidelity simulation |
17:00 - 17:30 | Applications of the discrete viscous adjoint method for aerodynamic shape optimizations |
17:30 - 18:00 | An adjoint-based optimization method for helicopter backdoor geometry |
18:00 - 18:30 | Industrial application of the DLR TAU code to helicopter configurations at Eurocopter |
20:00 - Dinner
Wednesday, October 19, 2011
8:00 - 10:00 | 1st session Chair: Dieter Schwamborn (DLR-AS-CA) |
8:00 - 8:30 | Near-wall Reynolds stress modelling for RANS and hybrid RANS / LES methods |
8:30 - 9:00 | Aerodynamic resonance in transonic airfoil flow |
9:00 - 9:30 | Extensions for supersonic, reacting and high-enthalpy flows |
9:30 - 10:00 | ESA's activities using TAU within the field of aerothermodynamics and propulsion analysis |
10:00 - 10:30 - Coffee break & poster presentations
10:30 - 12:30 | 2nd session Chair: Andrew Peace (ARA) |
10:30 - 11:00 | Applications of TAU at MBDA-D |
11:00 - 11:30 | Industrial experiences with the TAU code for detached-eddy simulations |
11:30 - 12:00 | The DLR THETA code, the incompressible brother of TAU, an overview |
12:00 - 12:30 | The DLR TAU code: recent and future developments |
12:30 - 13:30 - Lunch
13:30 - 15:00 | Panel discussion |
15:00 - 15:10 | Conclusion |