Aerospace | Free Full-Text | On the Wake Properties of Segmented Trailing Edge Extensions
NACA 2424 (naca2424-il)
Applied Sciences | Free Full-Text | Aerodynamic Efficiency Improvement on a NACA-8412 Airfoil via Active Flow Control Implementation
計算工学ナビ
Biography Meng
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 0025 | 3D CAD Model Library | GrabCAD
計算工学ナビ
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
Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel - Page 8 of 21 - UNT Digital Library
The Effects of Airfoil Thickness on Dynamic Stall Characteristics of Highâ•'Solidity Vertical Axis Wind Turbines
Phase evolution of flow controlled by synthetic jets over NACA 0025 airfoil | SpringerLink
Phase evolution of flow controlled by synthetic jets over NACA 0025 airfoil | SpringerLink
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 16 of 21 - UNT Digital Library
![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
Experimental setup of NACA 0025 airfoil showing four ZNMF actuators, a... | Download Scientific Diagram
File:NACA 0025 a.svg - Wikimedia Commons
Comparison of pressure coefficient distribution of NACA 0025 airfoil... | Download Scientific Diagram
File:NACA 0025.svg - Wikimedia Commons
Comparison of numerical and experimental results over a NACA0025 airfoil undergoing separation
The Effects of Airfoil Thickness on Dynamic Stall Characteristics of Highâ•'Solidity Vertical Axis Wind Turbines
