Can I read NACA 0015 Airfoil Performance Data on EtoBox?
NACA 0015 Airfoil Performance Data by Deny Bayu Saefudin is a document available to read on EtoBox.
What is NACA 0015 Airfoil Performance Data about?
The document contains aerodynamic data for 31 points on an airfoil with a Reynolds number of 100,000, Mach number of 0.01, and forced transition on the top and bottom surfaces. It includes coefficients for lift (CL), drag (CD), pressure drag (CDp), pitching moment (Cm), and location of transition (Top Xtr and Bot Xtr) at angles of attack from -10 to 20 degrees.
- Author
- Deny Bayu Saefudin
- Language
- EN