Recent questions and answers in Thermal

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Considering the T-s diagram of Rayleigh flow and using the differential forms of the conservation equations

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Determine the mass flow rate, exit pressure, exit temperature, exit Mach number

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Assume that the flow through the nozzle is steady, one-dimensional and isentropic.

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Find the friction co-efficient of the duct in a adiabatic flow

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Determine the amount of heat added and the corresponding change in pressure.

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Explain properly, with the help of diagrams, what are the important conclusions derived from the above relationship

asked Nov 3, 2017 in Thermal by chandu (215k points)

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The reservoir pressure and the density is reduced by 37%.

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Estimate for an isothermal flow (i) the maximum length of pipe for no choking, (ii) the downstream conditions

asked Nov 3, 2017 in Thermal by chandu (215k points)

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How does a normal shock differ from an oblique shock?

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Prove that at the maximum entropy point Mach number is unity and all processes approach this point

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Considering isentropic flow in a nozzle show that

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Calculate the speed of the aircraft.

asked Nov 3, 2017 in Thermal by chandu (215k points)

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What is the time that elapses, by which the acoustic disturbance reaches an observer on the ground?

asked Nov 3, 2017 in Thermal by chandu (215k points)

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What is impulse function ?

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Determine the drop in total pressure of air in the combustion chamber.

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Determine the drop in total pressure of air in the combustion chamber.

asked Nov 3, 2017 in Thermal by chandu (215k points)

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What is a shock wave?

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Derive relation between stagnation and normal temperatures in a isotropic flow

asked Nov 3, 2017 in Thermal by chandu (215k points)

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The respective initial values for a compressible isentropic fluid flow past an immersed body.

asked Nov 3, 2017 in Thermal by chandu (215k points)

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Assume that the ratio of specific heat at constant pressure to that at constant volume

asked Nov 3, 2017 in Thermal by chandu (215k points)

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