Subsonic burning of fuel-air mixture producing steady pressure
Supersonic combustion producing a shock wave and sudden pressure rise
Use of turbines to compress the fuel-air mixture before ignition
Acceleration of exhaust gases through a convergent nozzle
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The Correct Option isB
Solution and Explanation
Step 1: Recall the meaning of detonation.
Detonation is a combustion process in which the flame propagates at supersonic speed.
Step 2: Identify its characteristics.
During detonation,
\[
\boxed{
\text{a shock wave is produced along with a sudden rise in pressure and temperature.}
}
\]
Therefore,
\[
\boxed{\text{Supersonic combustion producing a shock wave and sudden pressure rise}}
\]
is the correct answer.
Thus,
\[
\boxed{(B)}
\]
is the correct answer.