Summary report of the forces and moments over an NACA 0015 airfoil : through 180° angle of attack
The forces and moments over an NACA 0015 airfoil
1949
[2] Bl.
graph. Darst.
Book
English
Forces and moments over NACA 0015 airfoil through 180° angle of attack
Engineering Index Backfile | 1949
|Vortex Developments Over NACA 0015 Airfoil with Trailing Edge Jet
British Library Conference Proceedings | 1994
|Vortex Developments Over NACA 0015 Airfoil with Trailing Edge Jet
SAE Technical Papers | 1994
|