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Plz solve with answer clearly The force vectors on an aircraft are as shown. Find the net (resultant) force. T = Thrust L = Lift

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Plz solve with answer clearly

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The force vectors on an aircraft are as shown. Find the net (resultant) force. T = Thrust L = Lift D = Drag W = Weight The angle of Attack is degrees. Lift and Drag are also rotated degrees. L= 4193 T =7835 280 W -2980 D = 1123 Round each answer to two decimal places. Net (resultant) force: Net (resultant) direction (as an angle in degrees)

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