Local Skin-Friction Coefficient Formula:
From: | To: |
The Local Skin-Friction Coefficient (Cf) specifies the fraction of the local dynamic pressure that contributes to skin friction drag in fluid dynamics. It's a dimensionless parameter used to quantify the frictional resistance between a fluid and a solid surface.
The calculator uses the Local Skin-Friction Coefficient formula:
Where:
Explanation: The formula calculates the ratio of twice the shear stress to the product of static density and the square of static velocity, providing a measure of frictional drag relative to dynamic pressure.
Details: The skin-friction coefficient is crucial in aerodynamics and hydrodynamics for predicting drag forces, designing efficient vehicles and structures, and analyzing fluid flow behavior over surfaces.
Tips: Enter shear stress in Pascals, static density in kg/m³, and static velocity in m/s. All values must be positive and non-zero for accurate calculation.
Q1: What is the typical range of skin-friction coefficient values?
A: Skin-friction coefficients typically range from 0.001 to 0.01 for turbulent flow and can be even lower for laminar flow, depending on Reynolds number and surface conditions.
Q2: How does surface roughness affect the skin-friction coefficient?
A: Surface roughness generally increases the skin-friction coefficient by creating additional turbulence and disrupting the boundary layer flow.
Q3: What's the difference between local and average skin-friction coefficient?
A: Local skin-friction coefficient applies to a specific point on a surface, while average skin-friction coefficient represents the mean value over an entire surface area.
Q4: How does Reynolds number affect skin-friction coefficient?
A: For laminar flow, skin-friction coefficient decreases with increasing Reynolds number. For turbulent flow, it also decreases but at a different rate depending on the flow regime.
Q5: Can this formula be used for compressible flows?
A: This basic formula is primarily for incompressible flows. For compressible flows, additional factors such as Mach number and temperature variations need to be considered.