PPT - Airfoil Geometry Parameterization through Shape Optimizer and Computational Fluid Dynamics PowerPoint Presentation - ID:9335933
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NASA LS(1)-0417 profile used as baseline section for the wing models. | Download Scientific Diagram
![PDF] NASA low- and medium-speed airfoil development | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/a249494c6116794583a6d34813926568b6af9011/17-Figure8-1.png "PDF] NASA low- and medium-speed airfoil development | Semantic Scholar")
PDF] NASA low- and medium-speed airfoil development | Semantic Scholar
NASA LS(1)-0417 profile used as baseline section for the wing models. | Download Scientific Diagram
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