Self-noise of NACA 0012 and NACA 0021 aerofoils at the onset of stall - Alex Laratro, Maziar Arjomandi, Benjamin Cazzolato, Richard Kelso, 2017
![PDF] Experimental Analysis of a NACA 0021 Airfoil Under Dynamic Angle of Attack Variation and Low Reynolds Numbers | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/cb874787e3b07f8eaf847900288180a168109290/2-Figure2-1.png "PDF] Experimental Analysis of a NACA 0021 Airfoil Under Dynamic Angle of Attack Variation and Low Reynolds Numbers | Semantic Scholar")
PDF] Experimental Analysis of a NACA 0021 Airfoil Under Dynamic Angle of Attack Variation and Low Reynolds Numbers | Semantic Scholar
File:NACA 0021.svg - Wikimedia Commons
Numerical Analysis of the Influence of Airfoil Asymmetry on VAWT Performance
Experimental investigations of flow over NACA airfoils 0021 and 4412 of wind turbine blades with and without Tubercles - Usman Butt, Shafqat Hussain, Stephan Schacht, Uwe Ritschel, 2022
Performance Analysis of a H-Darrieus Wind Turbine for a Series of 4-Digit NACA Airfoils
AirfoilOrdinates_N
Comparison of lift and drag coefficients for NACA 0021 and NACA 65-021... | Download Scientific Diagram
NACA 0021 | Other | SimScale
The effect of undulating leading-edge modifications on NACA 0021 airfoil characteristics: Physics of Fluids: Vol 25, No 11
Effect of Leading-Edge Tubercle on Aerodynamic Performance of NACA 0021 Airfoil | SpringerLink
Vortex Shedding from NACA 0021 airfoil at 20 degrees incidence - YouTube
28: Tubercles effect on lift curve for NACA 0021 and NACA 65021 (HANSEN... | Download Scientific Diagram
NACA 0021 | Other | SimScale
Spectra of NACA 0012 and NACA 0021 airfoils at U ∞ = 30ms -1 | Download Scientific Diagram
Static and Dynamic Analysis of a NACA 0021 Airfoil Section at Low Reynolds Numbers: Drag and Moment Coefficients
NACA 0021 (naca0021-il)
Energies | Free Full-Text | Performance Analysis of a H-Darrieus Wind Turbine for a Series of 4-Digit NACA Airfoils
Clean Technol. | Free Full-Text | Strategies for Enhancing the Low Wind Speed Performance of H-Darrieus Wind Turbine—Part 1 | HTML
Testing of the Aerodynamic Characteristics of an Inflatable Airfoil Section | Journal of Aerospace Engineering | Vol 33, No 5
naca 0021 | 3D CAD Model Library | GrabCAD
2D CFD Simulation Study on the Performance of Various NACA Airfoils | CFD Letters
NACA airfoil - Wikipedia
NUMERICAL SIMULATION OF 4-DIGIT INCLINED NACA 00 XX AIRFOILS TO FIND OPTIMUM ANGLE OF ATTACK FOR AIRPLANE WING Haci SOGUKPINAR | Semantic Scholar
Comparison of lift and drag coefficients for NACA 0021 and NACA 65-021... | Download Scientific Diagram
Mean pressure and friction coefficients distributions over NACA 0021... | Download Scientific Diagram
Solution domain for NACA 0021 ( a ) and C-type structured mesh ( b ). | Download Scientific Diagram
