51): Effect of angle of attack, NACA-0025. | Download Scientific Diagram
Phase evolution of flow controlled by synthetic jets over NACA 0025 airfoil | SpringerLink
NACA0012, NACA0018, NACA0020, NACA0025 and NACA0030 blade profiles. | Download Scientific Diagram
Aerodynamic Benchmarking of the Deepwind Design
Effect of Blade Thickness of Vertical Axis Wind Turbine on Power Generation
File:NACA 0025 a.svg - Wikimedia Commons
File:NACA 0025.svg - Wikimedia Commons
Experimental setup of NACA 0025 airfoil showing four ZNMF actuators, a... | Download Scientific Diagram
![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
Experimental setup of NACA 0025 airfoil showing four ZNMF actuators, a... | Download Scientific Diagram
Phase evolution of flow controlled by synthetic jets over NACA 0025 airfoil | SpringerLink
Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel - Page 8 of 21 - UNT Digital Library
Biography Meng
Performance Analysis of Suction Airfoil and Computational Flow Visualization of Co-Flow Jet Airfoil
Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel - Page 15 of 21 - UNT Digital Library
NACA 0025 | 3D CAD Model Library | GrabCAD
NACA 0025 | 3D CAD Model Library | GrabCAD
NACA 0025 | 3D CAD Model Library | GrabCAD
Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel - Page 9 of 21 - UNT Digital Library
NACA 2424 (naca2424-il)
![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
Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel - UNT Digital Library
The Effects of Airfoil Thickness on Dynamic Stall Characteristics of Highâ•'Solidity Vertical Axis Wind Turbines
計算工学ナビ
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