Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 200+ more calculators!
Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
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11 Other formulas that you can solve using the same Inputs

Stanton number for hypersonic vehicle
Stanton Number=Local heat transfer rate/(static density*Static velocity*(Adiabatic wall enthalpy-Wall enthalpy)) GO
Adiabatic wall enthalpy using Stanton number
Adiabatic wall enthalpy=Local heat transfer rate/(static density*Static velocity*Stanton Number)+Wall enthalpy GO
Aerodynamic heating to the surface
Local heat transfer rate=static density*Static velocity*Stanton Number*(Adiabatic wall enthalpy-Wall enthalpy) GO
Static viscosity calculation using Chapman–Rubesin factor
static viscosity=(Density*Kinematic viscosity )/(Chapman–Rubesin factor*static density) GO
Static velocity equation using skin friction coefficient
Static velocity=sqrt((2*Shear Stress)/(Local skin-friction coefficient*static density)) GO
Static Density calculation using Chapman–Rubesin factor
static density=(Density*Kinematic viscosity )/(Chapman–Rubesin factor*static viscosity) GO
Chapman–Rubesin factor
Chapman–Rubesin factor=(Density*Kinematic viscosity )/(static density*static viscosity) GO
Static Density equation using skin friction coefficient
static density=(2*Shear Stress)/(Local skin-friction coefficient*(Static velocity^2)) GO
Viscosity calculation using Chapman–Rubesin factor
Kinematic viscosity =Chapman–Rubesin factor*static density*static viscosity/(Density) GO
Density calculation using Chapman–Rubesin factor
Density=Chapman–Rubesin factor*static density*static viscosity/(Kinematic viscosity ) GO
Local skin-friction coefficient
Local skin-friction coefficient=(2*Shear Stress)/(static density*(Static velocity^2)) GO

11 Other formulas that calculate the same Output

Shear stress on circular fillet weld subjected to Torsion
Shear Stress=2*Torque acting on rod/(pi*Throat thickness*Equivalent/Nominal Diameter of Particle^2) GO
Shear Stress When Dynamic Viscosity Of A Fluid Is Given
Shear Stress=Dynamic viscosity*(velocity of moving plate)/(distance between plates) GO
Shear Stress for long fillet weld subjected to torsion
Shear Stress=3*Torque acting on rod/(Throat thickness*(Length of weld^2)) GO
Shear stress produced if strain energy stored in a body due to shear stress is known
Shear Stress=sqrt((2*Modulus of rigidity*Strain Energy)/(Volume)) GO
Shear stress Produced if work done by gradually applied shear force is known
Shear Stress=sqrt((2*Modulus of rigidity*Work Done)/(Volume)) GO
Shear Stress due to torsional moment
Shear Stress=Torque*Distance/Polar moment of inertia GO
Shear-stress distribution.
Shear Stress=viscosity coefficient*Velocity Gradient GO
Shear stress if obliquity is given
Shear Stress=tan(angle of obliquity)*Normal stress GO
Shear stress if shear resistance is known
Shear Stress=Shear Resistance/Shear Area GO
Shear Stress of Circular Beam
Shear Stress=4*Shearing force/3*Area GO
Shear Stress
Shear Stress=Tangential Force/Area GO

local shear stress at the wall Formula

Shear Stress=(0.5)*Local skin-friction coefficient*static density*(static viscosity^2)
𝜏 =(0.5)*cf*ρ<sub>e</sub>*(μe^2)
More formulas
Local skin-friction coefficient GO
Static Density equation using skin friction coefficient GO
Static velocity equation using skin friction coefficient GO
Nusselt number for hypersonic vehicle GO
local heat-transfer rate using Nusselt's number GO
Thermal conductivity at the edge of the boundary layer equation using Nusselt's number GO
Stanton number for hypersonic vehicle GO
Adiabatic wall enthalpy using Stanton number GO
Nusselt's number with Reynolds number, the Stanton number and Prandtl number GO
Reynolds number for given Nusselt's number, Stanton number and Prandtl number GO
Stanton number with Reynolds number, Nusselt's number, Stanton number and Prandtl number GO
Prandtl number with Reynolds number, Nusselt's number, Stanton number and Stanton number GO
Skin friction coefficient for incompressible flow GO
viscosity around the wall GO

What is skin friction coefficient ?

The skin friction coefficient is an important dimensionless parameter in boundary-layer flows. It specifies the fraction of the local dynamic pressure, 0.5* ρ *μ ^2, that is felt as shear stress on the surface.

How to Calculate local shear stress at the wall?

local shear stress at the wall calculator uses Shear Stress=(0.5)*Local skin-friction coefficient*static density*(static viscosity^2) to calculate the Shear Stress, The local shear stress at the wall formula is defined as the product of half of the local skin friction coefficient, static density, and square of static velocity. Shear Stress and is denoted by 𝜏 symbol.

How to calculate local shear stress at the wall using this online calculator? To use this online calculator for local shear stress at the wall, enter Local skin-friction coefficient (cf), static density e) and static viscosity (μe) and hit the calculate button. Here is how the local shear stress at the wall calculation can be explained with given input values -> 5 = (0.5)*0.1*100000000*(0.001^2).

FAQ

What is local shear stress at the wall?
The local shear stress at the wall formula is defined as the product of half of the local skin friction coefficient, static density, and square of static velocity and is represented as 𝜏 =(0.5)*cf*ρe*(μe^2) or Shear Stress=(0.5)*Local skin-friction coefficient*static density*(static viscosity^2). Local skin-friction coefficient specifies the fraction of the local dynamic pressure, static density, is the density of the fluid when its not moving or the denity of fluid if we r moving relative to the fluid and static viscosity, is the viscosity of continuous flow, viscosity measures the ratio of the viscous force to the inertial force on the fluid.
How to calculate local shear stress at the wall?
The local shear stress at the wall formula is defined as the product of half of the local skin friction coefficient, static density, and square of static velocity is calculated using Shear Stress=(0.5)*Local skin-friction coefficient*static density*(static viscosity^2). To calculate local shear stress at the wall, you need Local skin-friction coefficient (cf), static density e) and static viscosity (μe). With our tool, you need to enter the respective value for Local skin-friction coefficient, static density and static viscosity and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Shear Stress?
In this formula, Shear Stress uses Local skin-friction coefficient, static density and static viscosity. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Shear Stress=2*Torque acting on rod/(pi*Throat thickness*Equivalent/Nominal Diameter of Particle^2)
  • Shear Stress=3*Torque acting on rod/(Throat thickness*(Length of weld^2))
  • Shear Stress=Tangential Force/Area
  • Shear Stress=4*Shearing force/3*Area
  • Shear Stress=Dynamic viscosity*(velocity of moving plate)/(distance between plates)
  • Shear Stress=Shear Resistance/Shear Area
  • Shear Stress=tan(angle of obliquity)*Normal stress
  • Shear Stress=viscosity coefficient*Velocity Gradient
  • Shear Stress=sqrt((2*Modulus of rigidity*Work Done)/(Volume))
  • Shear Stress=sqrt((2*Modulus of rigidity*Strain Energy)/(Volume))
  • Shear Stress=Torque*Distance/Polar moment of inertia
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