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
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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
Parallel upstream flow components after shock as Mach tends to infinite
Parallel upstream flow components =Velocity_of the fluid at 1*(1-(2*(sin(Wave angle))^2)/(Specific Heat Ratio-1)) GO
Perpendicular upstream flow components behind the shock wave
Perpendicular upstream flow components=Velocity_of the fluid at 1*((sin(2*Wave angle))/(Specific Heat Ratio-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
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 1 for a Steady Flow Formula

Cross sectional area=Discharge/(Density 1*Velocity_of the fluid at 1)
A=Q/(ρ<sub>1*V<sub>1)
More formulas
Mass Density at Section 1 for a Steady Flow GO
Velocity 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 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 1 for a Steady Flow?

Cross Sectional Area at Section 1 for a Steady Flow calculator uses Cross sectional area=Discharge/(Density 1*Velocity_of the fluid at 1) to calculate the Cross sectional area, The Cross Sectional Area at Section 1 for a Steady Flow 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 1 for a Steady Flow using this online calculator? To use this online calculator for Cross Sectional Area at Section 1 for a Steady Flow, enter Discharge (Q), Density 1 1) and Velocity_of the fluid at 1 (V1) and hit the calculate button. Here is how the Cross Sectional Area at Section 1 for a Steady Flow calculation can be explained with given input values -> 0.0002 = 1/(500*10).

FAQ

What is Cross Sectional Area at Section 1 for a Steady Flow?
The Cross Sectional Area at Section 1 for a Steady Flow formula is defined as sectional area at a particular point in the flow and is represented as A=Q/(ρ1*V1) or Cross sectional area=Discharge/(Density 1*Velocity_of the fluid at 1). Discharge is the rate of flow of a liquid, Density 1 is defined as the density of the fluid at point 1 and Velocity_of the fluid at 1 is defined as the velocity of the flowing liquid at a point 1.
How to calculate Cross Sectional Area at Section 1 for a Steady Flow?
The Cross Sectional Area at Section 1 for a Steady Flow formula is defined as sectional area at a particular point in the flow is calculated using Cross sectional area=Discharge/(Density 1*Velocity_of the fluid at 1). To calculate Cross Sectional Area at Section 1 for a Steady Flow, you need Discharge (Q), Density 1 1) and Velocity_of the fluid at 1 (V1). With our tool, you need to enter the respective value for Discharge, Density 1 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 Cross sectional area?
In this formula, Cross sectional area uses Discharge, Density 1 and Velocity_of the fluid at 1. 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
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