Engineering, 17.08.2021 02:30 miyahhh123
Assume a paved runway, and CLmax = 1.1 during the ground roll. When the airplane is on the ground, the wings are 1.2 m above the ground. Estimate the sea-level landing ground roll distance for the airplane. Assume that the airplane is landing with a weight of 2900 lb. The maximum lift coefficient with fl aps at touchdown is 1.8. After touchdown, assume zero lift.
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Assume a paved runway, and CLmax = 1.1 during the ground roll. When the airplane is on the ground, t...
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