Flow Reattachment on a NACA 0025 Airfoil Using an Array of Microblowers | AIAA Journal
Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel - Page 8 of 21 - UNT Digital Library
File:NACA 0025 a.svg - Wikimedia Commons
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Pressure distributions on the upper surface of the NACA 0025 airfoil when | Download Scientific Diagram
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File:NACA 0025.svg - Wikimedia Commons
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Applied Sciences | Free Full-Text | Aerodynamic Efficiency Improvement on a NACA-8412 Airfoil via Active Flow Control Implementation
![PDF] Fast Large Eddy Simulation of Flow Over a NACA 0025 at Low Reynolds Number | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/bf1aa42180a87efaeb1a6452a9f2aba17240c0a5/7-Figure2-1.png "PDF] Fast Large Eddy Simulation of Flow Over a NACA 0025 at Low Reynolds Number | Semantic Scholar")
PDF] Fast Large Eddy Simulation of Flow Over a NACA 0025 at Low Reynolds Number | Semantic Scholar
![PDF] Fast Large Eddy Simulation of Flow Over a NACA 0025 at Low Reynolds Number | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/bf1aa42180a87efaeb1a6452a9f2aba17240c0a5/8-Figure4-1.png "PDF] Fast Large Eddy Simulation of Flow Over a NACA 0025 at Low Reynolds Number | Semantic Scholar")
PDF] Fast Large Eddy Simulation of Flow Over a NACA 0025 at Low Reynolds Number | Semantic Scholar
Phase evolution of flow controlled by synthetic jets over NACA 0025 airfoil | SpringerLink
Performance Analysis of Suction Airfoil and Computational Flow Visualization of Co-Flow Jet Airfoil
Aerodynamic Benchmarking of the Deepwind Design
51): Effect of angle of attack, NACA-0025. | Download Scientific Diagram
![PDF] Wind tunnel evaluation of a truncated NACA 64-621 airfoil for wind turbine applications | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/e171eaebb262910f0dafd8e4f761a6fe463e1378/16-Figure1-1.png "PDF] Wind tunnel evaluation of a truncated NACA 64-621 airfoil for wind turbine applications | Semantic Scholar")
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Experimental setup of NACA 0025 airfoil showing four ZNMF actuators, a... | Download Scientific Diagram
Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel - Page 15 of 21 - UNT Digital Library
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Effect of Blade Thickness of Vertical Axis Wind Turbine on Power Generation
Aerospace | Free Full-Text | On the Wake Properties of Segmented Trailing Edge Extensions
Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel - Page 9 of 21 - UNT Digital Library
Numerical investigation of the effect of triangular cavity on the unsteady aerodynamics of NACA 0012 at a low Reynolds number - Rajesh Yadav, Aslesha Bodavula, 2022
Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel - UNT Digital Library
Experimental setup of NACA 0025 airfoil showing four ZNMF actuators, a... | Download Scientific Diagram
NACA 0025 | 3D CAD Model Library | GrabCAD
