www.cfd-online.com/Wiki/**Skin_friction_coefficient**

The skin friction coefficient, , is defined by: Where is the local wall shear stress, is the fluid density and is the free-stream velocity (usually taken ouside of the boundary layer or at the inlet).. For a turbulent boundary layer several approximation formulas for the local skin friction for a flat plate can be used:

**en.wikipedia.org**/wiki/**Skin_friction_drag**

The above equation, which is derived from Prandtl's one-seventh-power law, provided a reasonable approximation of the drag coefficient of low-Reynolds-number turbulent boundary layers. Compared to laminar flows, the skin friction coefficient of turbulent flows lowers more slowly as the Reynolds number increases. Skin friction drag

www.sciencedirect.com/.../**skin**-**friction**-**coefficient**

We first examine the accuracy of the momentum equation and compute the local skin-friction coefficients for a Reynolds number of 10 6 ≤ R x ≤ 10 9. We choose a unit Reynolds number of 1 × 10 6 (u e = 160 ft/sec, v = 1.6 × 10 –4 ft 2 /sec) and specify the flow as turbulent at x = 0.01 ft.

ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19940020691.pdf

implicit equation for the fully developed skin friction coefficient. To begin our analysis, we consider the shear stress closure by using Prandtl's mixing-length hypothesis The energy equation is approximately integrated by using the Crocco-Busemann relation (ref. 3) H = ClU + C2 (l) (2) assuming that Pr --1 and the pressure gradient is small.

naca.central.cranfield.ac.uk/reports/arc/rm/1874.pdf

momentum equation of the wake, the profile drag coefficient is then determined from equation (4). The calculations thus giv'eboth the total and skin friction drags, the difference is presumably the form drag. 3. Details of method--3.1.Laminar layer.-Tomotika'smethod is used to determine tIle skin ... and tIle local skin friction coefficient is ...

www.researchgate.net/post/**What_is_Skin_Friction_coefficient**

Hence, as far as it appears from the relation the Reynold no. is multiplied to the skin friction coefficient either to amplify or reduce effect of skin friction. To fit the value to scale of interest.

www.nuclear-power.net/.../**skin-friction-friction-drag**

It must be noted, the skin friction coefficient is equal to the Fanning friction factor.The Fanning friction factor, named after John Thomas Fanning, is a dimensionless number, that is one-fourth of the Darcy friction factor.As can be seen, there is a connection between skin friction forces and frictional head losses.. See also: Darcy Friction Factor ...

www.mne.psu.edu/.../pdf/**Flat_plate_turbulent_BL**.pdf

To these we add the integrated average skin friction coefficients for one side of a flat plate of length L, noting that Cf applies to the entire plate from x = 0 to x = L (see Chapter 11): Column (b) expressions are generally preferred for engineering analysis. Note that Cf, x is the local skin friction coefficient, applied at only one value of x.

**en.wikipedia.org**/wiki/**Parasitic_drag**

Parasitic drag is drag that results when an object is moved through a fluid medium. In the case of aerodynamic drag, the fluid medium is the atmosphere.Parasitic drag is a combination of form drag, skin friction drag and interference drag.The other components of total drag, induced drag, wave drag, and ram drag (see ram pressure), are separate types of drag, and are not components of parasitic ...

www.nuclear-power.net/.../**drag-force-drag-equation**

Drag Force – Drag Equation. The drag force, F D,depends on the density of the fluid, the upstream velocity, and the size, shape, and orientation of the body, among other things. One way to express this is by means of the drag equation.The drag equation is a formula used to calculate the drag force experienced by an object due to movement through a fluid.