An aircraft is equipped with a wing of symmetrical airfoils. The lift curve slope of the total aircraft is estimated to be 0CL/Oa = 5.0265 1/rad. The stall angle of attack (AOA) is 12°. Wing area is 16 m2. Use g = g0 and r = rO. What is the aircraft's mass during a flight on which a stall speed of 50 kt was observed?

Elements Of Electromagnetics
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Publisher:Sadiku, Matthew N. O.
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An aircraft is equipped with a wing of symmetrical

airfoils. The lift curve slope of the total aircraft is

estimated to be 0CL/Oa = 5.0265 1/rad. The stall

angle of attack (AOA) is 12°. Wing area is 16 m2.

Use g = g0 and r = rO.

What is the aircraft's mass during a flight on which

a stall speed of 50 kt was observed?

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