 Ch 9. External Flow Multimedia Engineering Fluids Drag Lift BoundaryLayer
 Chapter 1. Basics 2. Fluid Statics 3. Kinematics 4. Laws (Integral) 5. Laws (Diff.) 6. Modeling/Similitude 7. Inviscid 8. Viscous 9. External Flow 10. Open-Channel Appendix Basic Math Units Basic Equations Water/Air Tables Sections Search eBooks Dynamics Statics Mechanics Fluids Thermodynamics Math Author(s): Chean Chin Ngo Kurt Gramoll ©Kurt Gramoll FLUID MECHANICS - THEORY

In this section, the concept of drag will be introduced, and the concept of flow over an immersed body is illustrated with flow over a sphere. Flow around an Immersed Body: Drag
Click to view movie (44k) Frontal and Planform Areas
Click to view movie (52k) Wetted Area

Drag

When fluid flows over an immersed body, forces are exerted on that body. The resultant force parallel to the fluid motion is referred to as the drag. Determining drag is important in many engineering applications, such as the design of automobiles, airplanes, submarines and buildings.

Drag (D) consists of both friction and pressure drag, and it is often expressed in terms of a drag coefficient (CD) as

 D = CD ρAV2/2

where ρ is the fluid density; A is the characteristic area and V is the upstream velocity. The characteristic area can be choosen as: (a) the projected frontal area (often used for flow over automobiles and submarines), (b) the planform area (often used for flow over wings and hydrofoils), and (c) the wetted area (often used for flow over ships and barges). Hence, it is important to know which characteristic area was used when determining the drag coefficient.

Generally, the drag coefficient is determined through experiments, and it depends on parameters, such as the body shape, Reynolds number and surface roughness. The value of the drag coefficient for different body shapes subject to different flow conditions are available in the literature. Some of the drag coefficients for flow over two-dimensional and three-dimensional bodies are summarized in the following tables.

Drag Coefficient for
Two-Dimensional Body
 Shape Area, A Reynolds Number, Re Drag Coefficient CD Plate bD** > 104 2.0 Square bD > 104 2.1 Cylinder bD < 105 >5×105 1.2 (Laminar) 0.3 (Turbulent) Semicircular Cylinder  bD > 104 1.2 1.7 Hexagon bD > 104 1.0
(**Note: b is the length into the page)

Drag Coefficient for
Three
-Dimensional Body
 Shape Area, A Reynolds Number Re Drag Coefficient CD Cube D2 > 104 1.05 Hemisphere πD2/4 > 104 1.17 0.42 Cylinder πD2/4 > 104 L/D =0.5  => 1.10 L/D =1.0  => 0.93 L/D =2.0  => 0.83 L/D =4.0  => 0.85 Cone πD2/4 > 104 θ =10o  => 0.30 θ =30o  => 0.55 θ =60o  => 0.80 θ =90o  => 1.15

Flow over a Sphere Pressure Distribution for
Flow around a Sphere   Characteristics of Flow over Sphere Subject to Different Reynolds Numbers:
(a) Re << 1,
(b) 1×103 < Re < 2×105
(c) Re > 2×105 Drag Coefficient as a Function of the Reynolds Number for a Smooth Sphere

Consider flow over a sphere for illustration. Unlike flow over a flat plate, the pressure field of flow over a sphere is not uniform. This can be seen from the pressure distribution (i.e., ) around a sphere given in the figure.

At low Reynolds numbers (i.e., Re << 1), the viscous effects are important in a large area (shaded area). There is no flow separation, and the fluid is stuck to the sphere. The drag coefficient as a function of the Reynolds number is shown in the figure. At very small Reynolds numbers, Stokes has shown that the drag coefficient is a linear function of the Reynolds number, as given by

CD = 24/Re

At moderate Reynolds number (103 < Re < 2×105), a boundary layer is developed near the sphere. Viscous effects are important inside the region of this boundary layer. Due to the increase of the pressure drag, the fluid can no longer stick to the sphere, and it is separated at an angle (β) of about 80o. A broad wake region is formed downstreams. Note that the drag coefficient decreases with the Reynolds number, and it becomes almost a constant (CD = 0.4) for a Reynolds number between 103 and 2×105.

As the Reynolds number increases (Re > 2×105), the boundary layer becomes thinner in the front of the sphere and begins its transition to turbulent. The flow separation is delayed until an angle of about 120o, and the fluid forms a relatively narrow wake region in which the flow is highly unsteady and turbulent. For turbulent boundary layer flow, the drag coefficient is decreased further (e.g., CD = 0.06 for Re = 4×105). Hence, a turbulent boundary layer develops as fluid flows past an object will reduce the drag force. For example, the dimples of a golf ball (i.e., the surface roughness of the object) are used to create turbulent boundary layer flow, and hence reduce the drag force. Dimpled Golf Ball: Reduce Drag

Numerical Solutions to Low Reynolds Number Flows 