An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47° Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel
Author | : Ralph P. Bielat |
Publisher | : |
Total Pages | : 38 |
Release | : 1958 |
ISBN-10 | : OCLC:700933723 |
ISBN-13 | : |
Rating | : 4/5 ( Downloads) |
Book Synopsis An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47° Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel by : Ralph P. Bielat
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