Effects of systematically varying the spanwise and vertical location of an external store on the aerodynamic characteristics of an unswept tapered wing of aspect ratio 4 at Mach numbers of 1.41, 1.62, and 1.96
Description: Report presenting an investigation in the supersonic blowdown tunnel to determine the effects of an external store on the lift, drag, and pitching-moment characteristics of an unswept wing of aspect ratio 4 at Mach numbers of 1.41, 1.62, and 1.96.
Date: August 20, 1952
Creator: Jacobsen, Carl R.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department