The ratio of flight speed to the exhaust velocity for maximum propulsion efficiency is
(A) 0.0
(B) 0.5
(C) 1.0
(D) 2.0

Question ID - 156226 | SaraNextGen Top Answer

The ratio of flight speed to the exhaust velocity for maximum propulsion efficiency is
(A) 0.0
(B) 0.5
(C) 1.0
(D) 2.0