DESIGN|A|PLANE
Aerodynamics, Aircraft structures, Experimental
Saturday, February 7, 2009
NACA Technical note 2149
Investigation of boundary-layer control to improve the lift and drag characteristics of the NACA 65-2 415 airfoil section with double slotted and plain flaps
No comments:
Post a Comment
Newer Post
Older Post
Home
Subscribe to:
Post Comments (Atom)
No comments:
Post a Comment