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Option 4 : 1, 2 and 3 only
Explanation:
Shock waves:
- It has been found experimentally that, under some circumstances, it is possible for an almost spontaneous change to occur in a flow, with the velocity decreasing and pressure increasing through this region of sharp change.
- Such regions of sharp change can only occur if the initial flow is supersonic.
- The extremely thin region in which the transition from the initial supersonic waves, relatively low-pressure state to the state that involves low velocity, subsonic and high pressure is known as shock waves.
- A shock wave that is straight and at a right angle to the flow direction is known as Normal shock wave.
Across normal shock fluid properties change as follows:
- Velocity of flow decreases
- Pressure increases
- specific volume decreases
- Temperature increases
- Entropy increases
- Stagnation pressure decreases
- Density increases
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