Correct Answer : 15.8
Explanation : Power coefficient = 550*bhp / (density*diameter5*rps3)= 550*700 / (1.225*1.25*203) = 15.8.
Correct Answer : Option (D) : 90%
Explanation : Propeller efficiency = (thrust*velocity) / (bhp*550) = 1320*300/ (550*800) = 0.9 = 0.9*100 % = 90%.
Correct Answer : Option (D) : 0.813
Explanation : Thrust coefficient = Thrust / (density*diameter4*rps2) = 1000 / (1.225*1.24*222) = 0.813.
Correct Answer : Option (B) : 15.8