Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

A \(0.55\)-m-internal-diameter spherical tank made of 1 -cm-thick stainless steel \((k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) is used to store iced water at \(0^{\circ} \mathrm{C}\). The tank is located outdoors at $30^{\circ} \mathrm{C}\( and is subjected to winds at \)8 \mathrm{~km} / \mathrm{h}$. Assuming the entire steel tank to be at \(0^{\circ} \mathrm{C}\) and thus its thermal resistance to be negligible, determine \((a)\) the rate of heat transfer to the iced water in the tank and (b) the amount of ice at $0^{\circ} \mathrm{C}\( that melts during a \)24-\mathrm{h}$ period. The heat of fusion of water at atmospheric pressure is \(h_{i f}=333.7 \mathrm{~kJ} / \mathrm{kg}\). Disregard any heat transfer by radiation.

Short Answer

Expert verified
(a) The rate of heat transfer to the iced water in the tank is 2311.34 Watts. (b) The amount of ice at 0 degrees Celsius that melts during a 24-hour period is 604.13 kg.

Step by step solution

01

Find the properties of air at the film temperature

First, we have to find the properties of air. As the outdoor temperature is 30°C and the tank is at 0°C, the film temperature can be estimated as: $$T_f = \frac{T_\infty + T_s}{2} = \frac{30 + 0}{2} = 15 °C$$ From standard air property tables, we find that at 15°C: - Density \((\rho)\): 1.225 kg/m³ - Thermal conductivity \((k_a)\): 0.0242 W/(m·K) - Dynamic viscosity \((\mu)\): 1.81 x 10⁻⁵ kg/(m·s) - Specific heat at constant pressure \((C_p)\): 1006 J/(kg·K) - Kinematic viscosity \((\nu)\): 1.47 x 10⁻⁵ m²/s
02

Calculate wind velocity and Reynolds number

We need to convert wind velocity from km/h to m/s and find the Reynolds number to determine the flow regime. $$V = \frac{8 \mathrm{~km} / \mathrm{h}}{3.6} = 2.22 \mathrm{~m} / \mathrm{s}$$ The Reynolds number for flow over a sphere can be calculated as: $$Re = \frac{VD}{\nu} = \frac{2.22 * 0.55}{1.47 * 10^{-5}} = 83014$$ This is greater than 60000, which indicates a turbulent flow regime.
03

Calculate the Nusselt number using the Seider-Tate equation

To find the convection coefficient, we can now apply the empirical correlation (Seider-Tate equation) for turbulent flow over a sphere: $$Nu = 2 + \left [ 0.4(Re^{1/2})(Pr^{1/3}) \right ] + \left [ 0.06(Re^{2/3})(Pr^{1/3})(\frac{Pr}{Pr_s})^{1/4} \right ]$$ For air at the film temperature 15°C, the values are as follows: - Prandtl number \((Pr) = \frac{C_p\mu}{k_a} = \frac{1006 * 1.81 * 10^{-5}}{0.0242} = 0.712\) - Prandtl number at the surface temperature \((Pr_s) = 0.708\) (since air properties do not change much between 0°C and 15°C) Now substituting these values, we can find the Nusselt number: $$Nu = 2 + [0.4(83014^{1/2})(0.712^{1/3})] + [0.06(83014^{2/3})(0.712^{1/3})(\frac{0.712}{0.708})^{1/4}] = 214.34$$
04

Calculate the convection coefficient and the heat transfer rate

The convection coefficient \((h_c)\) is given by: $$h_c = \frac{Nu * k_a}{D} = \frac{214.34 * 0.0242}{0.55} = 9.37 \mathrm{~W} / (\mathrm{m}^2 \cdot \mathrm{K}) $$ Applying Newton's Law of Cooling for the convective heat transfer, we can find the rate of heat transfer: $$Q = h_c A\Delta T = h_c * 4\pi r^2 (T_\infty - T_s) = 9.37 * 4 * \pi * (0.275)^2 * (30 - 0) = 2311.34 \mathrm{~W}$$ Thus, the rate of heat transfer to the iced water in the tank is 2311.34 Watts. (a)
05

Calculate the melted ice during a 24-hour period

The heat of fusion of water \((h_{if})\) is given as 333.7 kJ/kg. Now, the energy required to melt a mass (\(m\)) of ice per day can be calculated by: $$E = m * h_{if} = 2311.34 \mathrm{~W} * 86400 \mathrm{~s}$$ Rearranging and solving for mass, we get: $$m = \frac{2311.34 * 86400}{333.7 * 1000} = 604.13 \mathrm{~kg}$$ Therefore, 604.13 kg of ice at 0 degrees Celsius melts during a 24-hour period. (b)

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

A \(15-\mathrm{mm} \times 15-\mathrm{mm}\) silicon chip is mounted such that the edges are flush in a substrate. The chip dissipates \(1.4 \mathrm{~W}\) of power uniformly, while air at \(20^{\circ} \mathrm{C}\) ( $\left.1 \mathrm{~atm}\right)\( with a velocity of \)25 \mathrm{~m} / \mathrm{s}$ is used to cool the upper surface of the chip. If the substrate provides an unheated starting length of \(15 \mathrm{~mm}\), determine the surface temperature at the trailing edge of the chip. Evaluate the air properties at $50^{\circ} \mathrm{C}$.

Consider laminar flow over a flat plate. Will the friction coefficient change with distance from the leading edge? How about the heat transfer coefficient?

Hot carbon dioxide exhaust gas at \(1 \mathrm{~atm}\) is being cooled by flat plates. The gas at \(220^{\circ} \mathrm{C}\) flows in parallel over the upper and lower surfaces of a \(1.5\)-m-long flat plate at a velocity of $3 \mathrm{~m} / \mathrm{s}$. If the flat plate surface temperature is maintained at \(80^{\circ} \mathrm{C}\), determine \((a)\) the local convection heat transfer coefficient at \(1 \mathrm{~m}\) from the leading edge, \((b)\) the average convection heat transfer coefficient over the entire plate, and (c) the total heat flux transfer to the plate.

Hot water vapor flows in parallel over the upper surface of a 1-m-long plate. The velocity of the water vapor is \(10 \mathrm{~m} / \mathrm{s}\) at a temperature of \(450^{\circ} \mathrm{C}\). A coppersilicon (ASTM B98) bolt is embedded in the plate at midlength. The maximum use temperature for the ASTM B98 copper-silicon bolt is \(149^{\circ} \mathrm{C}\) (ASME Code for Process Piping, ASME B31.3-2014, Table A-2M). To devise a cooling mechanism to keep the bolt from getting above the maximum use temperature, it becomes necessary to determine the local heat flux at the location where the bolt is embedded. If the plate surface is kept at the maximum use temperature of the bolt, what is the local heat flux from the hot water vapor at the location of the bolt?

Engine oil at \(85^{\circ} \mathrm{C}\) flows over a \(10-\mathrm{m}\)-long flat plate whose temperature is \(35^{\circ} \mathrm{C}\) with a velocity of $2.5 \mathrm{~m} / \mathrm{s}$. Determine the total drag force and the rate of heat transfer over the entire plate per unit width.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free