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Define frontal area of a body subjected to external flow. When is it appropriate to use the frontal area in drag and lift calculations?

Short Answer

Expert verified
The frontal area of a body subjected to external flow is the area of the body that faces the flow, being perpendicular to the flow direction. It is the "shadow" of the body as seen in a plane projecting the geometric outline of the object in the direction of the flow. It is appropriate to use the frontal area in drag and lift calculations when considering the shape of the body, the effects of fluid viscosity, streamlined bodies in motion, and incompressible flow situations. The frontal area helps in better understanding the interaction of the body with the fluid medium and calculating forces correctly.

Step by step solution

01

Definition of Frontal Area

The frontal area of a body subjected to external flow is the area of the body that faces the flow, i.e., the area that is perpendicular to the direction of the flow. It is the "shadow" of the body as seen in a plane projecting the geometric outline of the object in the direction of the flow. The frontal area is important in determining the drag and lift forces experienced by the body when subjected to a fluid flow.
02

Appropriate Use of Frontal Area in Drag and Lift Calculations

Frontal area plays a significant role in calculating drag and lift forces acting on a body in fluid flow. The drag force is the force that acts opposite to the direction of the flow, while lift force acts perpendicular to the direction of the flow. It is appropriate to use the frontal area in drag and lift calculations when: 1. The shape of the body in the flow affects the flow separation and consideration of the whole body geometry becomes necessary. 2. The effect of fluid viscosity on forces should be taken into account. 3. We are considering the forces acting on streamlined bodies moving through a fluid. 4. The flow is incompressible because high pressure occurs only on the front part of the body. In these cases, it is essential to use the frontal area to determine the overall force acting on the body due to the fluid flow (drag or lift). The frontal area helps in better understanding the interaction of the body with the fluid medium and calculating forces correctly. In summary, the frontal area is the area of a body facing the fluid flow direction, and it is appropriate to use it in drag and lift calculations when we need to consider the shape of the body, the effects of fluid viscosity, the consideration of streamlined bodies in motion, and when dealing with incompressible flow situations.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

External Flow
External flow refers to the stream of fluid that moves around a solid object. Imagine the wind flowing around a building, or water flowing past a ship. That's external flow in action. This type of flow can occur in gases or liquids and often leads to various forces like drag and lift, which affect the object immersed in the flow.

External flow is significant in many real-world applications. From engineers designing car bodies for aerodynamics to understanding how birds fly, knowing how fluid moves around objects helps in optimizing efficiency and performance. In essence, external flow dictates how the flow field interacts with surfaces, which can lead to energy loss or pressure changes.
Drag Force
Drag force is the resistance force caused by the motion of a body through a fluid. Have you felt the wind pushing against you as you ride a bike? That's drag force. This force acts in the opposite direction to the motion of the object.

There are several components contributing to drag force:
  • Friction Drag: Comes from the fluid sliding past the surface of the body.
  • Pressure Drag: Caused by a difference in pressure between the front and rear of the object.
Drag is influenced by the object's shape and speed, the fluid's density, and even the roughness of the object's surface. Reducing drag is crucial in engineering to save energy, improve speed and efficiency, and even reduce fuel consumption.
Lift Force
Lift force is a force that acts perpendicular to the motion of a body moving through a fluid. It is lift that allows airplanes to rise into the air and birds to soar through the skies.

Achieving lift involves several factors:
  • Angle of Attack: The angle at which the flow meets the object significantly influences lift.
  • Shape of the Object: Certain shapes can redirect airflow to generate more lift.
  • Flow Velocity: Faster streams of flow can increase lift significantly.
Understanding lift force is essential in designing wings or blades that are capable of lifting aircraft or generating energy in wind turbines. It is a pivotal concept in fields like aerodynamics and fluid dynamics.
Fluid Flow Calculations
Fluid flow calculations are essential for predicting how fluids behave in different scenarios. They involve using mathematical equations and principles to determine values like flow velocity, pressure changes, and forces such as drag and lift.

These calculations are based on core fluid dynamics principles:
  • Bernoulli’s Equation: Relates pressure, velocity, and height in fluid flow phenomena.
  • Continuity Equation: Ensures mass conservation in fluid flow systems.
  • Navier-Stokes Equations: Provide a comprehensive model for fluid motion.
Precision in fluid flow calculations is vital in designing systems that efficiently transfer fluids, such as pipelines, HVAC systems, and even aerodynamic designs. Through these calculations, engineers can predict the behavior of fluids and optimize systems for better performance.

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Most popular questions from this chapter

Why is flow separation in flow over cylinders delayed in turbulent flow?

A \(0.2 \mathrm{~m} \times 0.2 \mathrm{~m}\) street sign surface has an absorptivity of \(0.6\) and an emissivity of \(0.7\), while the street sign is subjected to a cross flow wind at \(20^{\circ} \mathrm{C}\) with a velocity of \(1 \mathrm{~m} / \mathrm{s}\). Solar radiation is incident on the street sign at a rate of \(1100 \mathrm{~W} / \mathrm{m}^{2}\), and the surrounding temperature is \(20^{\circ} \mathrm{C}\). Determine the surface temperature of the street sign. Evaluate the air properties at \(30^{\circ} \mathrm{C}\). Treat the sign surface as a vertical plate in cross flow.

Air at \(15^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\) flows over a \(0.3\)-m-wide plate at \(65^{\circ} \mathrm{C}\) at a velocity of \(3.0 \mathrm{~m} / \mathrm{s}\). Compute the following quantities at \(x=x_{\mathrm{cr}}\) : (a) Hydrodynamic boundary layer thickness, \(\mathrm{m}\) (b) Local friction coefficient (c) Average friction coefficient (d) Total drag force due to friction, \(\mathrm{N}\) (e) Local convection heat transfer coefficient, \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (f) Average convection heat transfer coefficient, W/m² \(\cdot \mathrm{K}\) (g) Rate of convective heat transfer, W

Air at \(15^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\) flows over a \(0.3\)-m-wide plate at \(65^{\circ} \mathrm{C}\) at a velocity of \(3.0 \mathrm{~m} / \mathrm{s}\). Compute the following quantities at \(x=0.3 \mathrm{~m}\) : (a) Hydrodynamic boundary layer thickness, \(\mathrm{m}\) (b) Local friction coefficient (c) Average friction coefficient (d) Total drag force due to friction, \(\mathrm{N}\) (e) Local convection heat transfer coefficient, W/m² \(\mathbf{K}\) (f) Average convection heat transfer coefficient, W/m² \(\mathrm{K}\) (g) Rate of convective heat transfer, W

Consider a refrigeration truck traveling at \(55 \mathrm{mph}\) at a location where the air temperature is \(80^{\circ} \mathrm{F}\). The refrigerated compartment of the truck can be considered to be a 9-ft-wide, 8-ft-high, and 20 -ft-long rectangular box. The refrigeration system of the truck can provide 3 tons of refrigeration (i.e., it can remove heat at a rate of \(600 \mathrm{Btu} / \mathrm{min}\) ). The outer surface of the truck is coated with a low-emissivity material, and thus radiation heat transfer is very small. Determine the average temperature of the outer surface of the refrigeration compartment of the truck if the refrigeration system is observed to be operating at half the capacity. Assume the air flow over the entire outer surface to be turbulent and the heat transfer coefficient at the front and rear surfaces to be equal to that on side surfaces. For air properties evaluations assume a film temperature of \(80^{\circ} \mathrm{F}\). Is this a good assumption?

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