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Define incompressible flow and incompressible fluid. Must the flow of a compressible fluid necessarily be treated as compressible?

Short Answer

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Answer: An incompressible flow is a fluid flow in which the density of the fluid remains constant throughout, meaning that any volume of the fluid will maintain its mass and fluctuations in pressure or temperature will not cause significant changes in its density. An incompressible fluid is a fluid whose density does not change significantly under pressure or temperature variations. The flow of a compressible fluid cannot always be treated as compressible. In some cases, when the changes in density resulting from pressure and temperature variations are negligible, the flow can be treated as incompressible. This simplification is valid if the Mach number (ratio of the flow velocity to the speed of sound) is low, which is typically considered to be less than 0.3. When the Mach number is greater than 0.3, the density changes cannot be ignored, and the flow must be treated as compressible.

Step by step solution

01

Define incompressible flow

An incompressible flow is a type of fluid flow in which the density of the fluid remains constant throughout. This means that any volume of this fluid will maintain its mass and the fluctuations in pressure or temperature will not cause any significant changes in its density.
02

Define incompressible fluid

An incompressible fluid refers to a fluid whose density does not change significantly with the application of pressure or temperature variations. It's important to note that no real fluid is truly incompressible, but some fluids can be considered as incompressible over a certain range of conditions, where the changes in density are negligible. Common examples include water and air at low speeds and low pressure variations.
03

Address the compressible fluid flow treatment

In some cases, the flow of a compressible fluid can be treated as incompressible when the changes in density resulting from pressure and temperature variations are negligible. This simplification is valid if the Mach number (ratio of the flow velocity to the speed of sound) is low, which is typically considered to be less than 0.3. When the Mach number is greater than 0.3, the density changes cannot be ignored, and the flow must be treated as compressible.

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Most popular questions from this chapter

Will a thermal boundary layer develop in flow over a surface even if both the fluid and the surface are at the same temperature?

The upper surface of an ASME SB-96 coppersilicon plate is subjected to convection with hot air flowing at \(6.5 \mathrm{~m} / \mathrm{s}\) parallel over the plate surface. The plate is square with a length of \(1 \mathrm{~m}\), and the temperature of the hot air is \(200^{\circ} \mathrm{C}\). The ASME Boiler and Pressure Vessel Code (ASME BPVC.IV-2015, HF-300) limits equipment constructed with ASME SB-96 plate to be operated at a temperature not exceeding \(93^{\circ} \mathrm{C}\). From a wind tunnel experiment, the average friction coefficient for the upper surface of the plate was found to be \(0.0023\). In the interest of designing a cooling mechanism to keep the plate surface temperature from exceeding \(93^{\circ} \mathrm{C}\), determine the minimum heat removal rate required to keep the plate surface from going above \(93^{\circ} \mathrm{C}\). Use the following air properties for the analysis: $c_{p}=1.016 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}, k=0.03419 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, \)\mu=2.371 \times 10^{-5} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\(, and \)\rho=0.8412 \mathrm{~kg} / \mathrm{m}^{3}$.

Air flows over a flat plate at $40 \mathrm{~m} / \mathrm{s}, 25^{\circ} \mathrm{C}\(, and \)1 \mathrm{~atm}\( pressure. \)(a)$ What plate length should be used to achieve a Reynolds number of \(1 \times 10^{8}\) at the end of the plate? (b) If the critical Reynolds number is \(5 \times 10^{5}\), at what distance from the leading edge of the plate would transition occur?

In an effort to prevent the formation of ice on the surface of a wing, electrical heaters are embedded inside the wing. With a characteristic length of \(2.5 \mathrm{~m}\), the wing has a friction coefficient of \(0.001\). If the wing is moving at a speed of \(200 \mathrm{~m} / \mathrm{s}\) through air at $1 \mathrm{~atm}\( and \)-20^{\circ} \mathrm{C}$, determine the heat flux necessary to keep the wing surface above \(0^{\circ} \mathrm{C}\). Evaluate the air properties at \(-10^{\circ} \mathrm{C}\) and 1 atm.

Two metal plates are connected by a long ASTM B 98 copper-silicon bolt. A hot gas at \(200^{\circ} \mathrm{C}\) flows between the plates and across the cylindrical bolt. The diameter of the bolt is \(9.5 \mathrm{~mm}\), and the length of the bolt exposed to the hot gas is \(10 \mathrm{~cm}\). The average convection heat transfer coefficient for the bolt in crossflow is correlated with the gas velocity as \(h=24.6 \mathrm{~V}^{0.62}\), where \(h\) and \(V\) have the units \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and $\mathrm{m} / \mathrm{s}$, respectively. The maximum use temperature for the ASTM B98 bolt is \(149^{\circ} \mathrm{C}\) (ASME Code for Process Piping, ASME B31.3-2014, Table A-2M). If the gas velocity is \(10.4 \mathrm{~m} / \mathrm{s}\), determine the minimum heat removal rate required to keep the bolt surface from going above the maximum use temperature.

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