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(Solved): desing an aerodinamically corrected horizontal stabilizer for the aircraft in the picture, knowing i ...



desing an aerodinamically corrected horizontal stabilizer for the aircraft in the picture, knowing its following data
wing surface= 10.3 cm2
aspect ratio= 7.5
taper ratio= 0.8
twist angle= -3 degrees
incident angle= 1.5 degrees
airfoil= 2.5% of chamber
cruise speed= 50 m/s




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To design an aerodynamically corrected horizontal stabilizer for the aircraft, we'll consider the given data and follow a step-by-step approach. Please note that without access to the picture or specific aircraft parameters, the design will be based ...
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