Computational Fluid Dynamics Analysis of the Stall Characteristics of a Wing Designed Based on Prandtl’s Minimum Induced Drag
Author:
Affiliation:
1. NASA Armstrong Flight Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3009
Reference14 articles.
1. Overview and Summary of the Second AIAA High-Lift Prediction Workshop
2. Overview and Summary of the Third AIAA High Lift Prediction Workshop
3. Analysis of Stall Aerodynamics of a Swept Wing with Laminar-Flow Glove
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