An aircraft wing is experiencing AOA of 5°. If downwash due to wing is 2.6° then, how much angle is being seen by tail of the aircraft?

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1.	An aircraft wing is experiencing AOA of 5°. If downwash due to wing is 2.6° then, how much angle is being seen by tail of the aircraft?
A.	2.4°
B.	4.5°
C.	6.7°
D.	1.23°
Answer» B. 4.5°

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