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Consider a non-boiling gas-liquid two-phase flow in a \(102-\mathrm{mm}\) diameter tube, where the superficial gas velocity is one-third that of the liquid. If the densities of the gas and liquid are $\rho_{g}=8.5 \mathrm{~kg} / \mathrm{m}^{3}\( and \)\rho_{l}=855 \mathrm{~kg} / \mathrm{m}^{3}$, respectively, determine the flow quality and the mass flow rates of the gas and the liquid when the gas superficial velocity is $0.8 \mathrm{~m} / \mathrm{s}$.

Short Answer

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Question: Determine the flow quality and the mass flow rates of the gas and liquid when the gas superficial velocity is \(0.8 \mathrm{~m} / \mathrm{s}\) in a non-boiling gas-liquid two-phase flow in a tube with a diameter of 102 mm, where the superficial gas velocity is one-third that of the liquid. The densities of the gas and the liquid are 8.5 kg/m³ and 855 kg/m³, respectively. Answer: The flow quality is 0.25, the mass flow rate of the gas is 0.0551 kg/s, and the mass flow rate of the liquid is 16.6 kg/s.

Step by step solution

01

Calculate Superficial Liquid Velocity

Given that the superficial gas velocity is one-third that of the liquid, let's denote the superficial liquid velocity as \(V_l\). Then, the given relationship is: \(V_g = \frac{1}{3}V_l\) We are given the superficial gas velocity \(V_g = 0.8 \mathrm{~m} / \mathrm{s}\). Now we can solve for \(V_l\): \(V_l = 3V_g = 3 ( 0.8 \mathrm{~m} / \mathrm{s}) = 2.4 \mathrm{~m} / \mathrm{s}\) So the superficial liquid velocity is \(2.4 \mathrm{~m} / \mathrm{s}\).
02

Calculate Flow Quality

The flow quality \(x\) is defined as the ratio of superficial gas velocity to the total superficial velocity. Let's denote the total superficial velocity as \(V_T\). Then, we can find \(x\) as follows: \(V_T = V_g + V_l = 0.8 \mathrm{~m} / \mathrm{s} + 2.4 \mathrm{~m} / \mathrm{s} = 3.2 \mathrm{~m} / \mathrm{s}\) \(x = \frac{V_g}{V_T} = \frac{0.8 \mathrm{~m} / \mathrm{s}}{3.2 \mathrm{~m} / \mathrm{s}} = 0.25\) So the flow quality is \(0.25\).
03

Calculate Mass Flow Rates

The mass flow rate of the gas and the liquid can be determined using their respective velocities and densities. First, let's calculate the cross-sectional area of the tube, using the diameter \(D = 102~\mathrm{mm}\): \(A = \pi (\frac{D}{2})^2 = \pi (\frac{102 \times 10^{-3} \mathrm{~m}}{2})^2 = 0.008159 \mathrm{~m}^2\) Now, we can calculate the mass flow rates as follows: \(\dot{m}_g = \rho_g V_g A = 8.5 \mathrm{~kg} / \mathrm{m}^{3} \cdot 0.8 \mathrm{~m} / \mathrm{s} \cdot 0.008159 \mathrm{~m}^2 = 0.0551 \mathrm{~kg} / \mathrm{s}\) \(\dot{m}_l = \rho_l V_l A = 855 \mathrm{~kg} / \mathrm{m}^{3} \cdot 2.4 \mathrm{~m} / \mathrm{s} \cdot 0.008159 \mathrm{~m}^2 = 16.6 \mathrm{~kg} / \mathrm{s}\) So, the mass flow rate of the gas is \(0.0551 \mathrm{~kg} / \mathrm{s}\), and the mass flow rate of the liquid is \(16.6 \mathrm{~kg} / \mathrm{s}\).

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Most popular questions from this chapter

The condenser of a steam power plant operates at a pressure of $4.25 \mathrm{kPa}$. The condenser consists of 144 horizontal tubes arranged in a \(12 \times 12\) square array. The tubes are \(8 \mathrm{~m}\) long and have an outer diameter of \(3 \mathrm{~cm}\). If the tube surfaces are at $20^{\circ} \mathrm{C}\(, determine \)(a)$ the rate of heat transfer from the steam to the cooling water and (b) the rate of condensation of steam in the condenser. Answers: (a) \(5060 \mathrm{~kW}\), (b) \(2.06 \mathrm{~kg} / \mathrm{s}\)

Steam condenses at \(50^{\circ} \mathrm{C}\) on the tube bank consisting of 20 tubes arranged in a rectangular array of 4 tubes high and 5 tubes wide. Each tube has a diameter of \(3 \mathrm{~cm}\) and a length of \(5 \mathrm{~m}\), and the outer surfaces of the tubes are maintained at \(30^{\circ} \mathrm{C}\). The rate of condensation of steam is (a) \(0.12 \mathrm{~kg} / \mathrm{s}\) (b) \(0.28 \mathrm{~kg} / \mathrm{s}\) (c) \(0.31 \mathrm{~kg} / \mathrm{s}\) (d) \(0.45 \mathrm{~kg} / \mathrm{s}\) (e) \(0.62 \mathrm{~kg} / \mathrm{s}\) (For water, use $\rho_{l}=992.1 \mathrm{~kg} / \mathrm{m}^{3}, \mu_{l}=0.653 \times 10^{-3} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\(, \)\left.k_{t}=0.631 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, c_{p l}=4179 \mathrm{~J} / \mathrm{kg} \cdot{ }^{\circ} \mathrm{C}, h_{f g} \oplus T_{\omega}=2383 \mathrm{~kJ} / \mathrm{kg}\right)$

Consider a two-phase flow of air-water in a vertical upward stainless steel pipe with an inside diameter of \(0.0254\) \(\mathrm{m}\). The two-phase mixture enters the pipe at \(25^{\circ} \mathrm{C}\) at a system pressure of $201 \mathrm{kPa}\(. The superficial velocities of the water and air are \)0.3 \mathrm{~m} / \mathrm{s}\( and \)23 \mathrm{~m} / \mathrm{s}$, respectively. The differential pressure transducer connected across the pressure taps set $1 \mathrm{~m}\( apart records a pressure drop of \)2700 \mathrm{~Pa}$, and the measured value of the void fraction is \(0.86\). Using the concept of the Reynolds analogy, determine the two-phase convective heat transfer coefficient. Use the following thermophysical properties for water and air: $\rho_{l}=997.1 \mathrm{~kg} / \mathrm{m}^{3}, \mu_{l}=8.9 \times 10^{-4} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}, \mu_{s}=4.66 \times\( \)10^{-4} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}, \operatorname{Pr}_{l}=6.26, k_{l}=0.595 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \sigma=0.0719 \mathrm{~N} / \mathrm{m}\(, \)\rho_{g}=2.35 \mathrm{~kg} / \mathrm{m}^{3}$, and \(\mu_{g}=1.84 \times 10^{-5} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\).

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