Low-Order Method for Prediction of Separation and Stall on Unswept Wings
Author:
Affiliation:
1. North Carolina State University, Raleigh, North Carolina 27695-7910
Funder
Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.C036027
Reference81 articles.
1. XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils
2. DrelaM.YoungrenH. “Athena Vortex Lattice User Manual, Version 3.26,” 2006, http://web.mit.edu/drela/Public/web/avl/avl_doc.txt.
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