Accession Number : AD0011093


Title :   WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEEDS OF A SPOILER-SLOT- DEFLECTOR COMBINATION ON A NACA 65A006 WING WITH QUARTER-CHORD LINE SWEPT BACK 32.6


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA


Personal Author(s) : VOGLER, RAYMOND D


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/011093.pdf


Report Date : 29 May 1953


Pagination or Media Count : 30


Descriptors :   *AERODYNAMIC CHARACTERISTICS , *SWEPTBACK WINGS , *SPOILERS , WIND TUNNELS


Subject Categories : Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE