About this document
Aerodynamic Data for Symmetrical Airfoils by thadge is a document available to read on EtoBox.
This document summarizes wind tunnel test results for the aerodynamic characteristics of seven symmetrical airfoil sections from 0 to 180 degrees angle of attack for use in analyzing vertical axis wind turbines. Wind tunnel tests were conducted at moderate Reynolds numbers and provided force and moment data for four airfoils (NACA-0009, -0012, -0012H, and -0015) from 0 to 180 degrees angle of attack. The document also describes how an airfoil property synthesizer code can be used to extend the measured prop
- Author
- thadge
- Language
- EN