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

In flow over blunt bodies such as a cylinder, how does the pressure drag differ from the friction drag?

Short Answer

Expert verified
#tag_title# Short Answer #tag_content# The main difference between pressure drag and friction drag in the context of flow over blunt bodies is that pressure drag is typically more substantial for blunt bodies due to the early flow separation and larger pressure difference between the front and rear surfaces. In contrast, friction drag is less significant in blunt bodies, as pressure drag is the dominant force in these scenarios.

Step by step solution

01

Understand Pressure Drag

Pressure drag, also known as form drag, is the drag force resulting from the pressure differences on the front and rear surfaces of an object moving through a fluid. These pressure differences occur due to the separation of flow around the object, which creates a downstream wake of lower pressure. This wake produces a force on the object in the opposite direction of its motion, contributing to the overall drag.
02

Understand Friction Drag

Friction drag, also known as skin friction or viscous drag, is the force caused by the viscous resistance of the fluid against the object's surface. It is due to the shear stress generated by the fluid particles sliding past the object's surface. Friction drag is dependent on factors such as the fluid's viscosity, the object's surface roughness, and its shape.
03

Difference in Pressure Drag for Blunt Bodies

In the case of flow over blunt bodies, such as a cylinder, the pressure drag is significantly higher compared to that of streamlined objects, like an airfoil. This is because the flow separation occurs earlier for blunt bodies, causing a larger wake and a more significant pressure difference between the front and rear surfaces. The result is a higher pressure drag for blunt bodies.
04

Difference in Friction Drag for Blunt Bodies

The friction drag in flow over blunt bodies might be less pronounced than in streamlined bodies, depending on the specific geometry and flow conditions. However, in many situations, friction drag is relatively smaller in magnitude compared to pressure drag for blunt bodies, because pressure drag is the dominant and more significant force in these scenarios.
05

Compare Pressure Drag and Friction Drag for Blunt Bodies

For a blunt body like a cylinder, the pressure drag is typically more substantial than the friction drag. This is due to the flow separation and formation of a large low-pressure wake downstream, leading to a greater pressure difference between the front and rear surfaces of the object. In contrast, friction drag is usually less significant in blunt bodies compared to streamlined objects, where minimizing pressure drag is a primary design goal.

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 thin, square, flat plate has \(1.2 \mathrm{~m}\) on each side. Air at \(10^{\circ} \mathrm{C}\) flows over the top and bottom surfaces of a very rough plate in a direction parallel to one edge, with a velocity of $48 \mathrm{~m} / \mathrm{s}$. The surface of the plate is maintained at a constant temperature of \(54^{\circ} \mathrm{C}\). The plate is mounted on a scale that measures a drag force of \(1.5 \mathrm{~N}\). Determine the total heat transfer rate from the plate to the air.

Consider laminar flow of air across a hot circular cylinder. At what point on the cylinder will the heat transfer be highest? What would your answer be if the flow were turbulent?

Consider a house that is maintained at a constant temperature of $22^{\circ} \mathrm{C}$. One of the walls of the house has three single-pane glass windows that are \(1.5 \mathrm{~m}\) high and \(1.8 \mathrm{~m}\) long. The glass $(k=0.78 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( is \)0.5 \mathrm{~cm}$ thick, and the heat transfer coefficient on the inner surface of the glass is $8 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\(. Now winds at \)35 \mathrm{~km} / \mathrm{h}$ start to blow parallel to the surface of this wall. If the air temperature outside is \(-2^{\circ} \mathrm{C}\), determine the rate of heat loss through the windows of this wall. Assume radiation heat transfer to be negligible. Evaluate the air properties at a film temperature of $5^{\circ} \mathrm{C}\( and \)1 \mathrm{~atm}$.

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?

Hot engine oil at \(150^{\circ} \mathrm{C}\) is flowing in parallel over a flat plate at a velocity of \(2 \mathrm{~m} / \mathrm{s}\). Surface temperature of the \(0.5-\mathrm{m}\)-long flat plate is constant at \(50^{\circ} \mathrm{C}\). Determine (a) the local convection heat transfer coefficient at $0.2 \mathrm{~m}$ from the leading edge and the average convection heat transfer coefficient, and \((b)\) repeat part \((a)\) using the Churchill and Ozoe (1973) relation.

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