Aerodynamic Performance Improvements Due to Porosity in Wings at Moderate Re
Author:
Affiliation:
1. University of Southern California
Publisher
American Institute of Aeronautics and Astronautics
Reference22 articles.
1. Wind tunnel tests of wings at Reynolds numbers below 70 000
2. Experimental Studies of Separation on a Two-Dimensional Airfoil at Low Reynolds Numbers
3. On vortex shedding from an airfoil in low-Reynolds-number flows
4. The influence of laminar separation and transition on low Reynolds number airfoil hysteresis
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1. Effects of Perforated Plates on Shock Structure Alteration for NACA0012 Airfoils;Inventions;2024-03-05
2. Large-Eddy Simulation of Low-Reynolds-Number Flow Around Partially Porous Airfoils;Journal of Aircraft;2023-11
3. Unsteady aerodynamics of porous aerofoils;Journal of Fluid Mechanics;2021-02-24
4. Stepped Wings at Moderate Re with Implications on Multipoint Wing Design;AIAA Scitech 2020 Forum;2020-01-05
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