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- W315435101 abstract "Report presenting an investigation in the supersonic blowdown tunnel to determine the control characteristics of full-span trailing-edge spoilers on two related full-blunt wings with the same aspect ratio but differing angles of sweepback. A similar unswept wing that was larger and had a partially blunt trailing edge was also tested with a full-span trailing-edge spoiler. Results regarding the lift, rolling-moment, and pitching-moment coefficients for unswept wings, the 45-degree sweptback wing, and a comparison of spoiler data with flap data are provided." @default.
- W315435101 created "2016-06-24" @default.
- W315435101 creator A5060865939 @default.
- W315435101 date "1952-12-03" @default.
- W315435101 modified "2023-09-27" @default.
- W315435101 title "Control Characteristics of Trailing-edge Spoilers on Untapered Blunt Trailing-edge Wings of Aspect Ratio 2.7 with 0 Degree and 45 Degrees Sweepback at Mach Numbers of 1.41 and 1.96" @default.
- W315435101 hasPublicationYear "1952" @default.
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