Velocity 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%
✖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 [A]			+10% -10%
✖Density 2 is defined as the density of the fluid at point 2.ⓘ Density 2 [ρ_2]			+10% -10%

✖Initial Velocity at point 2 is the rate of change of its position with respect to a frame of reference and is a function of time.ⓘ Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given [u₀₂]

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

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

Stress at Point y for a Curved Beam

Stress=((Bending Moment )/(Cross sectional area*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

Bending Moment When Stress is Applied at Point y in a Curved Beam

Bending Moment =((Stress*Cross sectional area*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

Total Unit Stress in Eccentric Loading

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

Maximum Bending Moment when Maximum Stress For Short Beams is Given

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

Maximum Stress For Short Beams

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

Axial Load when Maximum Stress For Short Beams is Given

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

Electric Current when Drift Velocity is Given

Electric Current=Number of free charge particles per unit volume*[Charge-e]*Cross sectional area*Drift Velocity GO

Resistance

Resistance=(Resistivity*Length of Conductor)/Cross sectional area GO

Centrifugal Stress

Centrifugal Stress=2*Tensile Stress*Cross sectional area GO

Rate of Flow

Rate of flow=Cross sectional area*Average Velocity GO

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

Initial Velocity at point 2=Discharge/(Cross sectional area*Density 2)
u<sub>02</sub>=Q/(A*ρ<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

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

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

What is Velocity ?

The velocity of an object is the rate of change of its position with respect to a frame of reference, and is a function of time. Velocity is equivalent to a specification of an object's speed and direction of motion (e.g. 60 km/h to the north).

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

Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given calculator uses Initial Velocity at point 2=Discharge/(Cross sectional area*Density 2) to calculate the Initial Velocity at point 2, The Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given formula is defined as velocity of flow at a particular point in the stream. Initial Velocity at point 2 and is denoted by u₀₂ symbol.

How to calculate Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given using this online calculator? To use this online calculator for Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given, enter Discharge (Q), Cross sectional area (A) and Density 2 (ρ₂₎ and hit the calculate button. Here is how the Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given calculation can be explained with given input values -> 0.000143 = 1/(10*700).

FAQ

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

The Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given formula is defined as velocity of flow at a particular point in the stream and is represented as u₀₂=Q/(A*ρ₂₎ or Initial Velocity at point 2=Discharge/(Cross sectional area*Density 2). Discharge is the rate of flow of a liquid, 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 and Density 2 is defined as the density of the fluid at point 2.

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

The Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given formula is defined as velocity of flow at a particular point in the stream is calculated using Initial Velocity at point 2=Discharge/(Cross sectional area*Density 2). To calculate Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given, you need Discharge (Q), Cross sectional area (A) and Density 2 (ρ₂₎. With our tool, you need to enter the respective value for Discharge, Cross sectional area and Density 2 and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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