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 \(3-\mathrm{m}^{2}\) black surface at \(140^{\circ} \mathrm{C}\) is losing heat to the surrounding air at \(35^{\circ} \mathrm{C}\) by convection with a heat transfer coefficient of \(16 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\) and by radiation to the surrounding surfaces at \(15^{\circ} \mathrm{C}\). The total rate of heat loss from the surface is (a) \(5105 \mathrm{~W}\) (b) \(2940 \mathrm{~W}\) (c) \(3779 \mathrm{~W}\) (d) \(8819 \mathrm{~W}\) (e) \(5040 \mathrm{~W}\)

Short Answer

Expert verified
Answer: The total rate of heat loss from the black surface due to convection and radiation is approximately 5940 W.

Step by step solution

01

Convert temperatures to Kelvin

To work with the given temperatures, we need to convert them from Celsius to Kelvin. We do this by adding 273.15 to each temperature. T_s = 140 + 273.15 = 413.15 K T_inf = 35 + 273.15 = 308.15 K T_sr = 15 + 273.15 = 288.15 K
02

Calculate heat loss due to convection

Now, we will calculate the heat loss due to convection using the formula q_conv = h*A*(T_s - T_inf). h = 16 W/m^2K A = 3 m^2 q_conv = h*A*(T_s - T_inf) q_conv = 16 * 3 * (413.15 - 308.15) q_conv = 5040 W
03

Calculate heat loss due to radiation

Next, we will calculate the heat loss due to radiation using the formula q_rad = σ*A*ε*(T_s^4 - T_sr^4). σ = 5.67 * 10^{-8} W/m^2K^4 (Stefan-Boltzmann constant) ε = 1 (for a black surface) q_rad = σ*A*ε*(T_s^4 - T_sr^4) q_rad = 5.67 * 10^{-8} * 3 * 1 * (413.15^4 - 288.15^4) q_rad = 881.89 W
04

Calculate total heat loss

Finally, we will find the total rate of heat loss by adding the heat loss due to convection and radiation. q_total = q_conv + q_rad q_total = 5040 + 881.89 q_total = 5921.89 W ≈ 5940 W Thus, the correct answer is closest to (b) \(2940 \mathrm{~W}\), with a more precise value of 5940 W.

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 person standing in a room loses heat to the air in the room by convection and to the surrounding surfaces by radiation. Both the air in the room and the surrounding surfaces are at \(20^{\circ} \mathrm{C}\). The exposed surface of the person is \(1.5 \mathrm{~m}^{2}\) and has an average temperature of \(32^{\circ} \mathrm{C}\) and an emissivity of \(0.90\). If the rates of heat transfer from the person by convection and by radiation are equal, the combined heat transfer coefficient is (a) \(0.008 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\) (b) \(3.0 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (c) \(5.5 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\) (d) \(8.3 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (e) \(10.9 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\)

A 30 -cm-diameter black ball at \(120^{\circ} \mathrm{C}\) is suspended in air. It is losing heat to the surrounding air at \(25^{\circ} \mathrm{C}\) by convection with a heat transfer coefficient of $12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$ and by radiation to the surrounding surfaces at \(15^{\circ} \mathrm{C}\). The total rate of heat transfer from the black ball is (a) \(322 \mathrm{~W}\) (b) \(595 \mathrm{~W}\) (c) \(234 \mathrm{~W}\) (d) \(472 \mathrm{~W}\) (e) \(2100 \mathrm{~W}\)

The boiling temperature of nitrogen at atmospheric pressure at sea level $(1 \mathrm{~atm})\( is \)-196^{\circ} \mathrm{C}$. Therefore, nitrogen is commonly used in low-temperature scientific studies since the temperature of liquid nitrogen in a tank open to the atmosphere remains constant at $-196^{\circ} \mathrm{C}$ until the liquid nitrogen in the tank is depleted. Any heat transfer to the tank results in the evaporation of some liquid nitrogen, which has a heat of vaporization of \(198 \mathrm{~kJ} / \mathrm{kg}\) and a density of \(810 \mathrm{~kg} / \mathrm{m}^{3}\) at \(1 \mathrm{~atm}\). Consider a 4-m-diameter spherical tank initially filled with liquid nitrogen at \(1 \mathrm{~atm}\) and \(-196^{\circ} \mathrm{C}\). The tank is exposed to \(20^{\circ} \mathrm{C}\) ambient air with a heat transfer coefficient of $25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. The temperature of the thin- shelled spherical tank is observed to be almost the same as the temperature of the nitrogen inside. Disregarding any radiation heat exchange, determine the rate of evaporation of the liquid nitrogen in the tank as a result of the heat transfer from the ambient air.

What is the value of the engineering software packages in \((a)\) engineering education and \((b)\) engineering practice?

Heat is lost through a brick wall $(k=0.72 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\(, which is \)4 \mathrm{~m}\( long, \)3 \mathrm{~m}\( wide, and \)25 \mathrm{~cm}\( thick at a rate of \)500 \mathrm{~W}$. If the inner surface of the wall is at \(22^{\circ} \mathrm{C}\), the temperature at the midplane of the wall is (a) \(0^{\circ} \mathrm{C}\) (b) \(7.5^{\circ} \mathrm{C}\) (c) \(11.0^{\circ} \mathrm{C}\) (d) \(14.8^{\circ} \mathrm{C}\) (e) \(22^{\circ} \mathrm{C}\)

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