A prop driven A/C has BHP/W as 0.08. If density ratio is 0.2 and take – McqOptions

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1.	A prop driven A/C has BHP/W as 0.08. If density ratio is 0.2 and take off lift coefficient is 3 then find take-off parameter for the aircraft. Given wing loading W/s = 35.
A.	700
B.	800
C.	900
D.	500
Answer» B. 800

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