Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow 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%
✖Density 2 is defined as the density of the fluid at point 2.ⓘ Density 2 [ρ_2]			+10% -10%
✖Velocity_of the fluid at 2 is defined as the velocity of the flowing liquid at point 1.ⓘ Velocity_of the fluid at 2 [V_2]			+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 2 when flow at Section 1 for a Steady Flow 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!

Mridul Sharma

Indian Institute of Information Technology (IIIT), Bhopal

Mridul Sharma has verified this Calculator and 200+ more calculators!

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

Length of weir or notch for velocity of approach

Length=Discharge/((2/3)*coefficient of discharging*sqrt(2*[g])*(((initial height of liquid+final height of liquid)^1.5)-(final height of liquid^1.5))) GO

Equation of Continuity for Compressible Fluids

Velocity_of the fluid at 1=(Cross-Sectional area at a point 2*Velocity_of the fluid at 2*Density 2)/(Cross Sectional area 1*Density 1) GO

Equation of Continuity for Incompressible Fluids

Velocity_of the fluid at 1=(Cross-Sectional area at a point 2*Velocity_of the fluid at 2)/Cross Sectional area 1 GO

Cross-sectional area when Discharge is given from Manning's equation

Cross sectional area=(Discharge*Manning’s Roughness Coefficient)/(hydraulic radius^(2/3)*Bed Slope^(1/2)) GO

Slope of Gradient of the Stream bed when Discharge is given in Manning's equation

Bed Slope=((Discharge*Manning’s Roughness Coefficient)/(Cross sectional area*(hydraulic radius^2/3)))^2 GO

Hydraulic radius when Discharge is given in Manning equation

hydraulic radius=(Discharge*Manning’s Roughness Coefficient)/(Cross sectional area*Bed Slope^1/2)^(2/3) GO

Cease-to-flow Depth when Depth at the Gauging Station given

Cease-to-flow Depth=Depth at the Gauging Station-Head at the Control*(Discharge)-Terms of Order^2 GO

Depth at the Gauging Station

Depth at the Gauging Station=Cease-to-flow Depth+Head at the Control*(Discharge)+Terms of Order^2 GO

Length of weir or notch without velocity of approach

Length=Discharge/((2/3)*coefficient of discharging*sqrt(2*[g])*(initial height of liquid^1.5)) GO

Velocity of piston during retraction

Velocity=Discharge/(Area of piston-Area of piston rod) GO

Velocity of piston during extension

Velocity=Discharge/Area of piston 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 2 when flow at Section 1 for a Steady Flow is Given Formula

Cross sectional area=Discharge/(Density 2*Velocity_of the fluid at 2)
A=Q/(ρ<sub>2*V<sub>2)

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

Discharge through a Section for Steady Incompressible Fluid GO

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

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

What is Sectional Area ?

The cross-sectional area is the area of a two-dimensional shape that is obtained when a three-dimensional object - such as a cylinder - is sliced perpendicular to some specified axis at a point. For example, the cross-section of a cylinder - when sliced parallel to its base - is a circle.

How to Calculate Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given?

Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given calculator uses Cross sectional area=Discharge/(Density 2*Velocity_of the fluid at 2) to calculate the Cross sectional area, The Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given formula is defined as sectional area at a particular point in the flow. Cross sectional area and is denoted by A symbol.

How to calculate Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given using this online calculator? To use this online calculator for Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given, enter Discharge (Q), Density 2 (ρ₂₎ and Velocity_of the fluid at 2 (V₂₎ and hit the calculate button. Here is how the Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given calculation can be explained with given input values -> 0.000286 = 1/(700*5).

FAQ

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

The Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given formula is defined as sectional area at a particular point in the flow and is represented as A=Q/(ρ_2*V₂₎ or Cross sectional area=Discharge/(Density 2*Velocity_of the fluid at 2). Discharge is the rate of flow of a liquid, Density 2 is defined as the density of the fluid at point 2 and Velocity_of the fluid at 2 is defined as the velocity of the flowing liquid at point 1.

How to calculate Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given?

The Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given formula is defined as sectional area at a particular point in the flow is calculated using Cross sectional area=Discharge/(Density 2*Velocity_of the fluid at 2). To calculate Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given, you need Discharge (Q), Density 2 (ρ₂₎ and Velocity_of the fluid at 2 (V₂₎. With our tool, you need to enter the respective value for Discharge, Density 2 and Velocity_of the fluid at 2 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, Density 2 and Velocity_of the fluid at 2. 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!