Internal Combustion Engines
The basic requirement of a good combustion chamber is

High thermal efficiency and power output
Low compression ratio
Low volumetric efficiency
Minimum turbulence

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

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Internal Combustion Engines
The brake power (B.P.) of the engine is given by (where W = Brake load or dead load in newtons, l = Length of arm in meters, N = Speed of engine in r.p.m., S = Spring balance reading in newtons, D = Dia. of brake drum in meters, and d = Dia. of rope in meters)

P = (Wl × 2πN)/60 watts
P = [(W - S) π (D + d) N]/60 watts
P = [(W - S) πDN]/60 watts
All of these

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