An aircraft is to be designed to have max lift coefficient as 2.8 and – McqOptions

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1.	An aircraft is to be designed to have max lift coefficient as 2.8 and at q=10Pa. If maximum load factor n=5 then, what will be the stall speed?
A.	1.80m/s
B.	1.80mph
C.	2.80mph
D.	2.80m/s
Answer» B. 1.80mph

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