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
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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 2) 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 2). 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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