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What is the physical significance of the Prandtl number? Does the value of the Prandtl number depend on the type of flow or the flow geometry? Does the Prandtl number of air change with pressure? Does it change with temperature?

Short Answer

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Short Answer: The Prandtl number of air varies with temperature, as both the kinematic viscosity and thermal diffusivity of air increase with increasing temperature, but at different rates, typically causing the Prandtl number to increase. Pressure has a negligible effect on the Prandtl number for air, as it depends primarily on temperature. However, in non-ideal conditions such as very high pressures or non-equilibrium states, the Prandtl number may show minor changes with pressure.

Step by step solution

01

Physical Significance of Prandtl Number

The Prandtl number (Pr) is a dimensionless number used in fluid dynamics to describe the relative importance of viscous effects to thermal effects in a fluid flow. It is defined as: Pr = \frac{ν}{α} where ν is the kinematic viscosity, and α is the thermal diffusivity. A low Prandtl number indicates that the thermal diffusivity dominates, which means heat is transferred more efficiently than momentum. In contrast, a high Prandtl number signifies that the viscosity effects dominate, leading to slower heat transfer compared to momentum transfer.
02

Dependence on Flow Type and Flow Geometry

The Prandtl number is a property of the fluid and not related to the type of flow or flow geometry. Prandtl number only depends on the fluid's physical properties, such as its kinematic viscosity and thermal diffusivity. It remains constant for a particular fluid under given conditions, irrespective of the flow type (laminar or turbulent) or geometry.
03

Variation with Pressure

For an ideal gas, the Prandtl number does not change with pressure. This is because both kinematic viscosity and thermal diffusivity are functions of temperature only, making the Prandtl number only depend on the temperature for an ideal gas. However, air is not an ideal gas, and at very high pressures or when the air is not in thermodynamic equilibrium, some changes in Prandtl number can occur with pressure, but these changes are often insignificant.
04

Variation with Temperature

The Prandtl number of air does change with temperature. As the temperature increases, both the kinematic viscosity and thermal diffusivity of air increase, but their rates of increase are not equal. Typically, the kinematic viscosity increases more rapidly than the thermal diffusivity with increasing temperature, resulting in an increase in the Prandtl number of air. However, the relationship between Prandtl number and temperature is not linear, so it is often determined experimentally for various temperatures or by using correlations based on experimental data.

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Most popular questions from this chapter

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}$.

In turbulent flow, one can estimate the Nusselt number using the analogy between heat and momentum transfer (Colburn analogy). This analogy relates the Nusselt number to the coefficient of friction, \(C_{p}\) as (a) \(\mathrm{Nu}=0.5 C_{f} \operatorname{Re} \mathrm{Pr}^{1 / 3}\) (c) \(\mathrm{Nu}=C_{f} \operatorname{Re} \mathrm{Pr}^{1 / 3}\) (e) \(\mathrm{Nu}=C_{f} \operatorname{Re}^{1 / 2} \operatorname{Pr}^{1 / 3}\) (d) \(\mathrm{Nu}=C_{f} \operatorname{Re} P r^{2 / 3}\)

In any forced or natural convection situation, the velocity of the flowing fluid is zero where the fluid wets any stationary surface. The magnitude of heat flux where the fluid wets a stationary surface is given by (a) \(k\left(T_{\text {fluid }}-T_{\text {wall }}\right)\) (b) \(\left.k \frac{d T}{d y}\right|_{\text {wall }}\) (c) \(\left.k \frac{d^{2} T}{d y^{2}}\right|_{\text {wall }}\) (d) \(\left.h \frac{d T}{d y}\right|_{\text {wall }}\) (e) None of them

What is the physical significance of the Reynolds number? How is it defined for external flow over a plate of length \(L\) ?

An average man has a body surface area of \(1.8 \mathrm{~m}^{2}\) and a skin temperature of \(33^{\circ} \mathrm{C}\). The convection heat transfer coefficient for a clothed person walking in still air is expressed as $h=8.6 V^{0.53}\( for \)0.5

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