Numerical Simulation of DLR-F11 High Lift Configuration from HiLiftPW-2 using STAR-CCM+
Author:
Affiliation:
1. Computational Dynamics Ltd.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0914
Reference11 articles.
1. The aerodynamic design of multi-element high-lift systems for transport airplanes
2. Summary of the First AIAA CFD High-Lift Prediction Workshop
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1. Flow Analysis of the DLR-F11 High-Lift Model Using the Galatea-I Code;Journal of Aircraft;2018-01
2. Computational-Fluid-Dynamics Best Practices for Aircraft Wing-Tip Vortex Roll-Up;Journal of Aircraft;2017-07
3. Analysis of Low-Speed Stall Aerodynamics of a Swept Wing with Seamless Flaps;34th AIAA Applied Aerodynamics Conference;2016-06-10
4. Grid-Adapted FUN3D Computations for the Second High-Lift Prediction Workshop;Journal of Aircraft;2015-07
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