If CM0 is -0.052 and lift coefficient at zero angle CL0 is 0.92 then, – McqOptions

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1.	If CM0 is -0.052 and lift coefficient at zero angle CL0 is 0.92 then, find CMac. Consider rectangular wing.
A.	-0.282
B.	0.98
C.	2.5
D.	7.89
Answer» B. 0.98

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