Internal Combustion Engines
If V₁ is the jet velocity and V₀ is the vehicle velocity, then the propulsive efficiency of a rocket is given by

V₀/(V₀ + V₁)
V₁/(V₀ + V₁)
(V₀/V₁)/ [1 + (V₀/V₁)²]
[2(V₀/V₁)]/ [1 + (V₀/V₁)²]

ANSWER DOWNLOAD EXAMIANS APP

Internal Combustion Engines
For the same compression ratio

Otto cycle is more efficient than the Diesel
Both Otto and Diesel cycles are, equally efficient
Diesel cycle is more efficient than Otto
Compression ratio has nothing to do with efficiency

ANSWER DOWNLOAD EXAMIANS APP