What should be the load factor if, lift coefficient is designed as 2.1 – McqOptions

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1.	What should be the load factor if, lift coefficient is designed as 2.1 and aircraft is operating at dynamic pressure q as 20 Pa. Given W/s =12.
A.	3.5
B.	5.5
C.	3.25
D.	4.5
Answer» B. 5.5

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