Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given Calculator

Category	Engineering ↺
Engineering	Civil ↺
Civil	Hydraulics and Waterworks ↺
Hydraulics-And-Waterworks	Fundamentals of Fluid Flow ↺
Fundamentals-Of-Fluid-Flow	Continuity Equation ↺

✖Discharge is the rate of flow of a liquidⓘ Discharge [Q]			+10% -10%
✖Fluid velocity is the volume of fluid flowing in the given vessel per unit cross sectional area.ⓘ Fluid Velocity [u_f]			+10% -10%

✖Cross sectional area is the area of a two-dimensional shape that is obtained when a three dimensional shape is sliced perpendicular to some specifies axis at a point.ⓘ Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given [A]

⎘ Copy

👎 Report Issue!

👍 Share Now!

You are here:

Rithik Agrawal

National Institute of Technology Karnataka (NITK), Surathkal

Rithik Agrawal has created this Calculator and 400+ more calculators!

M Naveen

National Institute of Technology (NIT), Warangal

M Naveen has verified this Calculator and 100+ more calculators!

< 11 Other formulas that you can solve using the same Inputs

Stanton Number (using basic fluid properties)

Stanton Number=External convection heat transfer coefficient/(Specific Heat Capacity*Fluid Velocity*Density) GO

Heat Loss due to Pipe

Heat Loss due to Pipe=(Force*Length*Fluid Velocity^2)/(2*Diameter *Acceleration Due To Gravity) GO

Cavitation Number

Cavitation number=(Pressure-Vapour pressure)/(mass density*(Fluid Velocity^2)/2) GO

Head Loss due to friction

Head loss=Darcy friction factor*Fluid Velocity^(2)*Length/(Pipe Diameter*2*[g]) GO

Reynolds Number for Non-Circular Tubes

Reynolds Number=Density*Fluid Velocity*Characteristic Length/Dynamic viscosity GO

Reynolds Number

Reynolds Number=Liquid Density*Fluid Velocity*Pipe Diameter/Dynamic viscosity GO

Dynamic Pressure head-pitot tube

Dynamic Pressure head=(Fluid Velocity^(2))/(2*Acceleration Due To Gravity) GO

Reynolds Number for Circular Tubes

Reynolds Number=Density*Fluid Velocity*Diameter /Dynamic viscosity GO

Inertial Force Per Unit Area

Inertial Force per unit area=(Fluid Velocity^2)*Density GO

Dynamic Pressure

Dynamic Pressure=(Liquid Density*Fluid Velocity^(2))/2 GO

Turbulence

Turbulence=Density*Dynamic viscosity*Fluid Velocity GO

< 11 Other formulas that calculate the same Output

Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam

Cross sectional area=(Bending Moment /(Stress*Radius of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis)))) GO

Cross-Sectional Area when Axial Buckling Load for a Warped Section is Given

Cross sectional area=(Axial buckling Load*Polar moment of Inertia)/(Shear Modulus of Elasticity*Torsion constant+((pi^2)*Young's Modulus*Warping Constant/(Length^2))) GO

Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given

Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis))) GO

Cross-sectional area of the rod if stress induced in rod due to impact load is known

Cross sectional area=(2*Modulus Of Elasticity*Load Dropped(Impact Load)*Height through which load is dropped)/(Length of Rod*(Stress induced^2)) GO

Cross-Sectional Area when Elastic Critical Buckling Load is Given

Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus) GO

Cross-Sectional Area when Maximum Stress For Short Beams is Given

Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) GO

Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given

Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity) GO

Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given

Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant) GO

Cross-Sectional Area when Critical Buckling Load for Pin Ended Columns is Given

Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus) GO

Total Cross-Sectional Area of Tensile Reinforcing

Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam) GO

Area when water flow equation is given

Cross sectional area=water flow/flow velocity GO

Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given Formula

Cross sectional area=Discharge/Fluid Velocity
A=Q/u<sub>f</sub>

More formulas

Mass Density at Section 1 for a Steady Flow GO

Velocity at Section 1 for a Steady Flow GO

Cross Sectional Area at Section 1 for a Steady Flow GO

Mass Density at Section 2 when flow at Section 1 for a Steady Flow is Given GO

Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given GO

Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given GO

Discharge through a Section for Steady Incompressible Fluid GO

Velocity at Section when Discharge through a Section for Steady Incompressible Fluid is Given GO

What is Equation of Continuity ?

A continuity equation in physics is an equation that describes the transport of some quantity. It is particularly simple and powerful when applied to a conserved quantity, but it can be generalized to apply to any extensive quantity.

How to Calculate Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given?

Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given calculator uses Cross sectional area=Discharge/Fluid Velocity to calculate the Cross sectional area, The Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given is defined as sectional area of pipe. Cross sectional area and is denoted by A symbol.

How to calculate Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given using this online calculator? To use this online calculator for Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given, enter Discharge (Q) and Fluid Velocity (u_f) and hit the calculate button. Here is how the Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given calculation can be explained with given input values -> 1 = 1/1.

FAQ

What is Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given?

The Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given is defined as sectional area of pipe and is represented as A=Q/u_f or Cross sectional area=Discharge/Fluid Velocity. Discharge is the rate of flow of a liquid and Fluid velocity is the volume of fluid flowing in the given vessel per unit cross sectional area.

How to calculate Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given?

The Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given is defined as sectional area of pipe is calculated using Cross sectional area=Discharge/Fluid Velocity. To calculate Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given, you need Discharge (Q) and Fluid Velocity (u_f). With our tool, you need to enter the respective value for Discharge and Fluid Velocity 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 Cross sectional area?

In this formula, Cross sectional area uses Discharge and Fluid Velocity. We can use 11 other way(s) to calculate the same, which is/are as follows -

Cross sectional area=(Bending Moment /(Stress*Radius of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis))))
Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia))
Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis)))
Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus)
Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus)
Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant)
Cross sectional area=(Axial buckling Load*Polar moment of Inertia)/(Shear Modulus of Elasticity*Torsion constant+((pi^2)*Young's Modulus*Warping Constant/(Length^2)))
Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam)
Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity)
Cross sectional area=(2*Modulus Of Elasticity*Load Dropped(Impact Load)*Height through which load is dropped)/(Length of Rod*(Stress induced^2))
Cross sectional area=water flow/flow velocity

Facebook
Twitter
WhatsApp
Reddit
LinkedIn
E-Mail

Let Others Know

✖

Facebook

Twitter

Copied!