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

What is heat flux? How is it related to the heat transfer rate?

Short Answer

Expert verified
Question: Define heat flux and explain its relation to heat transfer rate. Answer: Heat flux is defined as the rate of heat transfer per unit area of a surface and is denoted by 'q'. It is measured in Watts per square meter (W/m²). The heat transfer rate, denoted by 'Q', represents the amount of heat energy transferred across a surface in a given time and is measured in Watts (W). The relationship between heat flux and heat transfer rate can be derived by considering the area (A) over which the heat transfer is taking place. The formula to establish this relationship is q = Q / A, where q is the heat flux, Q is the heat transfer rate, and A is the area over which the heat transfer is occurring.

Step by step solution

01

Define heat flux

Heat flux, denoted by 'q', is defined as the rate of heat transfer per unit area of a surface. It represents the amount of thermal energy that passes through a certain area in a given time. The units for heat flux are Watts per square meter (W/m²).
02

Define heat transfer rate

Heat transfer rate, denoted by 'Q', is the amount of heat energy transferred across a surface in a given time. It is typically measured in Watts (W), where 1 Watt is equivalent to 1 Joule of energy transferred per second (1 W = 1 J/s).
03

Understand the relationship between heat flux and heat transfer rate

To establish the relationship between heat flux (q) and heat transfer rate (Q), we need to take into account the area (A) over which the heat transfer is taking place. The heat flux is the heat transfer rate per unit area, which means that the heat transfer rate is equal to the heat flux multiplied by the area.
04

Derive the formula for the relationship between heat flux and heat transfer rate

We know that heat transfer rate (Q) is equal to heat flux (q) multiplied by the area (A). We can write this relationship mathematically as: Q = q × A Now we can see the relationship between heat flux and heat transfer rate. Heat flux (q) can be calculated by dividing the heat transfer rate (Q) by the area (A): q = \frac{Q}{A} In conclusion, heat flux is the rate of heat transfer per unit area, and it is related to the heat transfer rate through the formula q = Q / A, where q is the heat flux, Q is the heat transfer rate, and A is the area over which heat transfer is taking place.

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

Why is it necessary to ventilate buildings? What is the effect of ventilation on energy consumption for heating in winter and for cooling in summer? Is it a good idea to keep the bathroom fans on all the time? Explain.

Which expression is used to determine the heat flux emitted by thermal radiation from a surface? (a) \(-k A \frac{d T}{d x}\) (b) \(-k \operatorname{grad} T\) (c) \(h\left(T_{2}-T_{1}\right)\) (d) \(\varepsilon \sigma T^{4}\) (e) None of them

The outer surface of a spacecraft in space has an emissivity of \(0.8\) and a solar absorptivity of \(0.3\). If solar radiation is incident on the spacecraft at a rate of \(950 \mathrm{~W} / \mathrm{m}^{2}\), determine the surface temperature of the spacecraft when the radiation emitted equals the solar energy absorbed.

An aluminum pan whose thermal conductivity is $237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\( has a flat bottom with diameter \)15 \mathrm{~cm}$ and thickness \(0.4 \mathrm{~cm}\). Heat is transferred steadily to boiling water in the pan through its bottom at a rate of \(800 \mathrm{~W}\). If the inner surface of the bottom of the pan is at \(105^{\circ} \mathrm{C}\), determine the temperature of the outer surface of the bottom of the pan.

Consider steady heat transfer between two large parallel plates at constant temperatures of \(T_{1}=290 \mathrm{~K}\) and \(T_{2}=150 \mathrm{~K}\) that are \(L=2 \mathrm{~cm}\) apart. Assuming the surfaces to be black (emissivity \(\varepsilon=1\) ), determine the rate of heat transfer between the plates per unit surface area assuming the gap between the plates is \((a)\) filled with atmospheric air, \((b)\) evacuated, \((c)\) filled with fiberglass insulation, and \((d)\) filled with superinsulation having an apparent thermal conductivity of \(0.00015 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\).

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