Results from the Second AIAA CFD High-Lift Prediction Workshop Using Edge
Author:
Affiliation:
1. Department of Aeronautics and Systems Technology, Swedish Defence Research Agency, SE-164 90 Stockholm, Sweden
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032899
Reference23 articles.
1. Evaluation of CFD methods for transport aircraft high lift systems
2. The European High Lift Project EUROLIFT II - Objectives, Approach, and Structure
3. Low Speed High Lift Validation Tests Within the European Project EUROLIFT II
4. von GeyrH.SchadeN.van der BurgJ. W.EliassonP.EsquieuS. “CFD Prediction of Maximum Lift Effects on Realistic High-Lift-Commercial-Aircraft-Configurations Within the European project EUROLIFT II,” AIAA Paper 2007-4299, June 2007.
5. Transition Prediction and Impact on 3D High-Lift Wing Configuration
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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. Efficient stall compliance prediction method for trimmed very light aircraft with high-lift devices;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2016-05-16
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