DESIGN|A|PLANE
Aerodynamics, Aircraft structures, Experimental
Showing posts with label
NACA 65
.
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Showing posts with label
NACA 65
.
Show all posts
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
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