Chapter 17: Problem 13
In which medium will sound travel fastest for a given temperature: air, helium, or argon?
Chapter 17: Problem 13
In which medium will sound travel fastest for a given temperature: air, helium, or argon?
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Get started for freeProducts of combustion enter a gas turbine with a stagnation pressure of \(0.75 \mathrm{MPa}\) and a stagnation temperature of \(690^{\circ} \mathrm{C}\), and they expand to a stagnation pressure of \(100 \mathrm{kPa}\) Taking \(k=1.33\) and \(R=0.287 \mathrm{kJ} / \mathrm{kg} \cdot \mathrm{K}\) for the products of combustion, and assuming the expansion process to be isentropic, determine the power output of the turbine per unit mass flow.
A gas initially at a subsonic velocity enters an adiabatic diverging duct. Discuss how this affects (a) the velocity, ( \(b\) ) the temperature, (c) the pressure, and (d) the density of the fluid.
What is sound? How is it generated? How does it travel? Can sound waves travel in a vacuum?
It is claimed that an oblique shock can be analyzed like a normal shock provided that the normal component of velocity (normal to the shock surface) is used in the analysis. Do you agree with this claim?
Air is flowing in a wind tunnel at \(12^{\circ} \mathrm{C}\) and \(66 \mathrm{kPa}\) at a velocity of \(230 \mathrm{m} / \mathrm{s}\). The Mach number of the flow is (a) \(0.54 \mathrm{m} / \mathrm{s}\) \((b) 0.87 \mathrm{m} / \mathrm{s}\) \((c) 3.3 \mathrm{m} / \mathrm{s}\) \((d) 0.36 \mathrm{m} / \mathrm{s}\) \((e) 0.68 \mathrm{m} / \mathrm{s}\)
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