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

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
Neutral Axis to Outermost Fiber Distance when Total Unit Stress in Eccentric Loading is Given
Outermost Fiber Distance=(Total Unit Stress-(Axial Load/Cross sectional area))*Moment of Inertia about Neutral Axis/(Axial Load*Distance_from Load Applied) 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
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

2 Other formulas that calculate the same Output

Density of the fluid for stagnation considering compressible fluid flow
Density 1=Stagnation density /((1+(((Specific Heat Ratio-1)/2)*(Local Mach number^2)))^(1/(Specific Heat Ratio-1))) GO
Density of fluid considering velocity at outlet of orifice
Density 1=(2*Specific Heat Ratio*Pressure at inlet)/((Velocity of flow at outlet^2)*(Specific Heat Ratio+1)) GO

Mass Density at Section 1 for a Steady Flow Formula

Density 1=Discharge/(Cross sectional area*Velocity_of the fluid at 1)
ρ<sub>1=Q/(A*V<sub>1)
More formulas
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
Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given GO

What is Density ?

The density, of a substance is its mass per unit volume. The symbol most often used for density is ρ, although the Latin letter D can also be used. Mathematically, density is defined as mass divided by volume.

How to Calculate Mass Density at Section 1 for a Steady Flow?

Mass Density at Section 1 for a Steady Flow calculator uses Density 1=Discharge/(Cross sectional area*Velocity_of the fluid at 1) to calculate the Density 1, The Mass Density at Section 1 for a Steady Flow formula is defined as density of fluid at a point or mass per unit volume at a point in a flow. Density 1 and is denoted by ρ1 symbol.

How to calculate Mass Density at Section 1 for a Steady Flow using this online calculator? To use this online calculator for Mass Density at Section 1 for a Steady Flow, enter Discharge (Q), Cross sectional area (A) and Velocity_of the fluid at 1 (V1) and hit the calculate button. Here is how the Mass Density at Section 1 for a Steady Flow calculation can be explained with given input values -> 0.01 = 1/(10*10).

FAQ

What is Mass Density at Section 1 for a Steady Flow?
The Mass Density at Section 1 for a Steady Flow formula is defined as density of fluid at a point or mass per unit volume at a point in a flow and is represented as ρ1=Q/(A*V1) or Density 1=Discharge/(Cross sectional area*Velocity_of the fluid at 1). 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 Velocity_of the fluid at 1 is defined as the velocity of the flowing liquid at a point 1.
How to calculate Mass Density at Section 1 for a Steady Flow?
The Mass Density at Section 1 for a Steady Flow formula is defined as density of fluid at a point or mass per unit volume at a point in a flow is calculated using Density 1=Discharge/(Cross sectional area*Velocity_of the fluid at 1). To calculate Mass Density at Section 1 for a Steady Flow, you need Discharge (Q), Cross sectional area (A) and Velocity_of the fluid at 1 (V1). With our tool, you need to enter the respective value for Discharge, Cross sectional area and Velocity_of the fluid at 1 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 Density 1?
In this formula, Density 1 uses Discharge, Cross sectional area and Velocity_of the fluid at 1. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Density 1=Stagnation density /((1+(((Specific Heat Ratio-1)/2)*(Local Mach number^2)))^(1/(Specific Heat Ratio-1)))
  • Density 1=(2*Specific Heat Ratio*Pressure at inlet)/((Velocity of flow at outlet^2)*(Specific Heat Ratio+1))
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