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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Q. What is the Mach number at room temperature?

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Q. In a one-dimensional flow, the gas flows through one spatial dimension, namely its length.

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Q. The compressible flow is assumed to be _____________

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Q. Ratio of duct length to width length in a compressible flow is_______

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Q. The fluid speed through the nozzle is altered with________

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