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A wing (NA 23015) with a surface area of m² and area, is tested in a wind tunnel (ρar = 1.2kg/m³). What is the replace
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A wing (NA 23015) with a surface area of m² and area, is tested in a wind tunnel (ρar = 1.2kg/m³). What is the replace
A wing (NA 23015) with a surface area of m² and area, istested in a wind tunnel (ρar =1.2kg/m³). What is the replacement for this created wing whenpositioned with the attack design α andto a wind with V m/s. For this same attack project you drag it tocalculate aboutthis wing. Also calculate the maintenance and the maximum for thisto create as a condition in this conditionof maximum lift. (To solve this question, assign values to X, Vand α)
1,8 1,6 1,4 CD 1,2 CL 1,0 0,8 0,6 0,4 0,2 0,020 0,016 0,012 0,008 0,004 T T CL1,724 Sconventional section (NACA 23015) a I 8 12 16 4 angle of attack angle of attack . conventional section (NACA 23015) 8 a grade 12 16 1, a (grade 20 20
1,8 1,6 1,4 CD 1,2 CL 1,0 0,8 0,6 0,4 0,2 0,020 0,016 0,012 0,008 0,004 T T CL1,724 Sconventional section (NACA 23015) a I 8 12 16 4 angle of attack angle of attack . conventional section (NACA 23015) 8 a grade 12 16 1, a (grade 20 20