Q. Shocks generated due to trailing exothermic reaction is called ______

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Q. __________ is referred as the temperature at a stagnation point in the flow of fluids in fluid mechanics and thermodynamics.

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Q. In ________ and _______ kind of flow, the stagnation temperature is equal to the total temperature.

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Q. _____ is the law employed in the derivation of stagnation point.

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Q. A bimetallic ________ is generally utilized to measure stagnation temperature.

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Q. Stagnation point is the point in fluid mechanics where the velocity of the fluid at that point is _____

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Q. _________ proves that the static pressure is maximum when the velocity is zero.

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Q. Total pressure is an addition of static pressure and ______

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Q. The pressure coefficient at a stagnation point is _____

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Q. _________ minus freestream static pressure gives freestream dynamic pressure.

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Q. On a streamlined body fully immersed in a potential flow, there are ____ stagnation points.

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Q. The exit velocity in the nozzle increases as per __________

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Q. With the increase in pressure, the exit velocity _________

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Q. Pumps increase __________

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Q. Which among the following is the formula for volumetric flow rate?

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Q. Which among the following is the formula for mass flow rate?

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Q. Compressible flow is a flow that deals with ______

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Q. Compressible flow mainly deals with _______

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Q. Which among the following is an assumption of the compressible flow?

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Q. What is Mach number?

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