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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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