Accession Number : ADA952025

Title :   A Low Speed Wind Tunnel Investigation of a 64-010 Airfoil Section with Nose Flat and Split Trailing Edge Flap,

Corporate Author : PRINCETON UNIV NJ DEPT OF AERONAUTICAL ENGINEERING

Personal Author(s) : Dike, D. J.

Report Date : 25 JUL 1955

Pagination or Media Count : 37

Descriptors :   *BOUNDARY LAYER CONTROL, *FLAPS(CONTROL SURFACES), AIRFOILS, NOSES, SPLIT FLAPS, TRAILING EDGES, LIFT, STALLING, PITCH(MOTION), LEADING EDGE FLAPS, SUBSONIC WIND TUNNELS.

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE