What is it about?
Wing or airfoil sections are susceptible to flow separation. Designing them while taking these effects into consideration is essential. A separation sensor is developed to limit separation by reducing it.
Featured Image
Read the Original
This page is a summary of: Airfoil Separation Constraint Formulation for Aerodynamic Shape Optimization, Journal of Aircraft, January 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c037365.
You can read the full text:
Contributors
Be the first to contribute to this page
