Contents
- 1 Which type of area would you use in the calculation of drag coefficient?
- 2 Does drag coefficient change with surface area?
- 3 What’s the least aerodynamic shape?
- 4 What is the best shape to reduce drag?
- 5 Which is more difficult to calculate, drag or lift?
- 6 How are drag coefficients determined in a wind tunnel?
Which type of area would you use in the calculation of drag coefficient?
reference area
Drag coefficients are almost always determined experimentally using a wind tunnel. Notice that the area (A) given in the drag equation is given as a reference area. The drag depends directly on the size of the body. Since we are dealing with aerodynamic forces, the dependence can be characterized by some area.
Does drag coefficient change with surface area?
The total aerodynamic force is equal to the pressure times the surface area around the body. Like the other aerodynamic force, lift, the drag is directly proportional to the area of the object. Doubling the area doubles the drag.
What is the reference area used for calculating drag coefficient of a cylinder?
Above a Reynolds number of 1000, the drag coefficient of the circular disk becomes a constant that has been consistently measured as 1.17. This coefficient is based upon a reference area equal to the frontal area of the disk, or π r² where r is the radius of the disk.
What’s the least aerodynamic shape?
It is generally accepted that some variation of the teardrop/airfoil shape has the lowest drag coefficient.
What is the best shape to reduce drag?
the best shape to reduce drag is streamline.
How does the reference area affect the drag coefficient?
As pointed out on the drag equation slide, the choice of reference area (wing area, frontal area, surface area.) will affect the actual numerical value of the drag coefficient that is calculated. When reporting drag coefficient values, it is important to specify the reference area that is used to determine the coefficient.
Which is more difficult to calculate, drag or lift?
D = Cd * A * .5 * r * V^2. For given air conditions, shape, and inclination of the object, we must determine a value for Cd to determine drag. Determining the value of the drag coefficient is more difficult than determining the lift coefficient because of the multiple sources of drag.
How are drag coefficients determined in a wind tunnel?
Drag coefficients are almost always determined experimentally using a wind tunnel. Notice that the area (A) given in the drag equation is given as a reference area. The drag depends directly on the size of the body.
How to calculate airfoil pressure and drag coefficient?
The drag coefficient then expresses the ratio of the drag force to the force produced by the dynamic pressure times the area. This equation gives us a way to determine a value for the drag coefficient.