Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped Calculator

Main Category	Engineering ↺
Engineering	Civil ↺
Civil	Hydraulics and Waterworks ↺
Hydraulics and Waterworks	Non-uniform Flow in Channels ↺
Non-uniform Flow in Channels	Surges in Open Channel Flow ↺
Surges in Open Channel Flow	Surge due to Sudden Reduction of Flow ↺

✖Absolute Velocity of the Issuing Jet is actual velocity of jet used in propeller.ⓘ Absolute Velocity of the Issuing Jet [V]			+10% -10%
✖Depth of Point 2 is the depth of point below the free surface in a static mass of liquid.ⓘ Depth of Point 2 [h ₂]			+10% -10%
✖Depth of Point 1 is the depth of point below the free surface in a static mass of liquid.ⓘ Depth of Point 1 [h ₁]			+10% -10%

✖Velocity_of the fluid at 1 is defined as the velocity of the flowing liquid at a point 1ⓘ Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped [V_1]

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Rithik Agrawal

National Institute of Technology Karnataka (NITK), Surathkal

Rithik Agrawal has created this Calculator and 1000+ more calculators!

Chandana P Dev

NSS College of Engineering (NSSCE), Palakkad

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Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped Solution

STEP 0: Pre-Calculation Summary

Formula Used

velocity_of_fluid_at_1 = (Absolute Velocity of the Issuing Jet*(Depth of Point 2-Depth of Point 1))/Depth of Point 1
V₁ = (V*(h ₂-h ₁))/h ₁
This formula uses 3 Variables

Variables Used

Absolute Velocity of the Issuing Jet - Absolute Velocity of the Issuing Jet is actual velocity of jet used in propeller. (Measured in Meter per Second)
Depth of Point 2 - Depth of Point 2 is the depth of point below the free surface in a static mass of liquid. (Measured in Meter)
Depth of Point 1 - Depth of Point 1 is the depth of point below the free surface in a static mass of liquid. (Measured in Meter)

STEP 1: Convert Input(s) to Base Unit

Absolute Velocity of the Issuing Jet: 10 Meter per Second --> 10 Meter per Second No Conversion Required
Depth of Point 2: 15 Meter --> 15 Meter No Conversion Required
Depth of Point 1: 10 Meter --> 10 Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

V₁ = (V*(h ₂-h ₁))/h ₁ --> (10*(15-10))/10

Evaluating ... ...

V₁ = 5

STEP 3: Convert Result to Output's Unit

5 Meter per Second --> No Conversion Required

FINAL ANSWER

5 Meter per Second <-- Velocity_of the fluid at 1

(Calculation completed in 00.031 seconds)

You are here

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

Efficiency of Propulsion when Head Loss Due to Friction is Given

efficiency = 2*Absolute Velocity of the Issuing Jet*Velocity of the Ship/((Absolute Velocity of the Issuing Jet+Velocity of the Ship)^2+2*[g]*Height) Go

Specific Weight of Liquid when Work Done by the Jet on Ship is Given

specific_weight_of_liquid = (Work *[g])/(Absolute Velocity of the Issuing Jet*Velocity of the Ship*Area) Go

Area of Issuing Jet when Work Done by the Jet on Ship is Given

area = (Work *[g])/(Absolute Velocity of the Issuing Jet*Velocity of the Ship*specific weight of liquid) Go

Efficiency of Propulsion

efficiency = 2*Absolute Velocity of the Issuing Jet*Velocity of the Ship/((Absolute Velocity of the Issuing Jet+Velocity of the Ship)^2) Go

Rate of Flow when Thrust on the Propeller is Given

rate_of_flow = Thrust force/(Water Density*(Absolute Velocity of the Issuing Jet-flow velocity)) Go

Weight of Water when Work Done by the Jet on Ship is Given

weight_of_water = (Work *[g])/(Absolute Velocity of the Issuing Jet*Velocity of the Ship) Go

Work Done by the Jet on Ship

work = weight of water*Velocity of the Ship*Absolute Velocity of the Issuing Jet/[g] Go

Velocity of the moving ship when Work Done by the Jet on Ship is Given

ship_velocity = (Work *[g])/(weight of water*Absolute Velocity of the Issuing Jet) Go

Weight of Water when Propelling Force is Given

weight_of_water = Force*[g]/Absolute Velocity of the Issuing Jet Go

Propelling Force

force = weight of water*Absolute Velocity of the Issuing Jet/[g] Go

Velocity of the Moving Ship when Relative Velocity is Given

ship_velocity = Relative Velocity-Absolute Velocity of the Issuing Jet Go

< 11 Other formulas that calculate the same Output

Velocity at Depth1 when Absolute velocity of the surge moving towards right is Given

velocity_of_fluid_at_1 = Absolute Velocity of the Issuing Jet-sqrt(([g]*Depth of Point 2*(Depth of Point 2+Depth of Point 1))/(2*Depth of Point 1)) Go

Velocity at Depth1 when Celerity of the Wave is Given

velocity_of_fluid_at_1 = ((([g]*(Depth of Point 2+Depth of Point 1))/(2*Depth of Point 1))*Height/Celerity of the Wave)+Velocity_of the fluid at 2 Go

Velocity at Depth1 when Absolute velocity of the surge moving towards right is Given

velocity_of_fluid_at_1 = ((Absolute Velocity of the Issuing Jet*(Depth of Point 1-Depth of Point 2))+(Velocity_of the fluid at 2*Depth of Point 2))/Depth of Point 1 Go

Velocity at Depth1 when Absolute velocity of the surge moving towards right is Given

velocity_of_fluid_at_1 = ((Absolute Velocity of the Issuing Jet*(Depth of Point 2-Depth of Point 1))+(Velocity_of the fluid at 2*Depth of Point 2))/Depth of Point 1 Go

Velocity at Outlet(Vw1) when Work Done on the Wheel per Second is given

velocity_of_fluid_at_1 = (((Work Done*specific gravity of liquid )/(Weight of Fluid*Angular Velocity))-(Velocity*Radius))/Radius 1 Go

Velocity at Outlet(Vw1) when Torque(T) Exerted by the Fluid is given

velocity_of_fluid_at_1 = (((Torque*specific gravity of liquid )/Weight of Fluid)-(Velocity*Radius))/Radius 1 Go

Equation of Continuity for Compressible Fluids

velocity_of_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

Velocity when Angular Momentum at Outlet is given

velocity_of_fluid_at_1 = (tangential momentum*specific gravity of liquid )/(Weight of Fluid*Radius 1) Go

Velocity at Depth1 when surge height is negligible

velocity_of_fluid_at_1 = (Height*[g]/Celerity of the Wave)+Velocity_of the fluid at 2 Go

Equation of Continuity for Incompressible Fluids

velocity_of_fluid_at_1 = (Cross-Sectional area at a point 2*Velocity_of the fluid at 2)/Cross Sectional area 1 Go

Velocity when Tangential Momentum of the Fluid Striking the Vanes at the Outlet is given

velocity_of_fluid_at_1 = (tangential momentum*specific gravity of liquid )/Weight of Fluid Go

Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped Formula

velocity_of_fluid_at_1 = (Absolute Velocity of the Issuing Jet*(Depth of Point 2-Depth of Point 1))/Depth of Point 1
V₁ = (V*(h ₂-h ₁))/h ₁

What is Absolute Velocity ?

The concept of absolute velocity is mainly used in turbomachinery design and defines the velocity of a fluid particle in relation to the surrounding, stationary environment. Together with the relative velocity (w) and the circumferential speed (u), it forms the velocity triangle.

How to Calculate Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped?

Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped calculator uses velocity_of_fluid_at_1 = (Absolute Velocity of the Issuing Jet*(Depth of Point 2-Depth of Point 1))/Depth of Point 1 to calculate the Velocity_of the fluid at 1, The Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped is defined as velocity at a particular depth. Velocity_of the fluid at 1 and is denoted by V₁ symbol.

How to calculate Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped using this online calculator? To use this online calculator for Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped, enter Absolute Velocity of the Issuing Jet (V), Depth of Point 2 (h ₂) and Depth of Point 1 (h ₁) and hit the calculate button. Here is how the Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped calculation can be explained with given input values -> 5 = (10*(15-10))/10.

FAQ

What is Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped?

The Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped is defined as velocity at a particular depth and is represented as V₁ = (V*(h ₂-h ₁))/h ₁ or velocity_of_fluid_at_1 = (Absolute Velocity of the Issuing Jet*(Depth of Point 2-Depth of Point 1))/Depth of Point 1. Absolute Velocity of the Issuing Jet is actual velocity of jet used in propeller, Depth of Point 2 is the depth of point below the free surface in a static mass of liquid and Depth of Point 1 is the depth of point below the free surface in a static mass of liquid.

How to calculate Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped?

The Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped is defined as velocity at a particular depth is calculated using velocity_of_fluid_at_1 = (Absolute Velocity of the Issuing Jet*(Depth of Point 2-Depth of Point 1))/Depth of Point 1. To calculate Velocity at Depth1 when Absolute velocity of the surge when the flow is completely stopped, you need Absolute Velocity of the Issuing Jet (V), Depth of Point 2 (h ₂) and Depth of Point 1 (h ₁). With our tool, you need to enter the respective value for Absolute Velocity of the Issuing Jet, Depth of Point 2 and Depth of Point 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 Velocity_of the fluid at 1?

In this formula, Velocity_of the fluid at 1 uses Absolute Velocity of the Issuing Jet, Depth of Point 2 and Depth of Point 1. We can use 11 other way(s) to calculate the same, which is/are as follows -

velocity_of_fluid_at_1 = (Cross-Sectional area at a point 2*Velocity_of the fluid at 2)/Cross Sectional area 1
velocity_of_fluid_at_1 = (Cross-Sectional area at a point 2*Velocity_of the fluid at 2*Density 2)/(Cross Sectional area 1*Density 1)
velocity_of_fluid_at_1 = (tangential momentum*specific gravity of liquid )/Weight of Fluid
velocity_of_fluid_at_1 = (tangential momentum*specific gravity of liquid )/(Weight of Fluid*Radius 1)
velocity_of_fluid_at_1 = (((Torque*specific gravity of liquid )/Weight of Fluid)-(Velocity*Radius))/Radius 1
velocity_of_fluid_at_1 = (((Work Done*specific gravity of liquid )/(Weight of Fluid*Angular Velocity))-(Velocity*Radius))/Radius 1
velocity_of_fluid_at_1 = ((Absolute Velocity of the Issuing Jet*(Depth of Point 1-Depth of Point 2))+(Velocity_of the fluid at 2*Depth of Point 2))/Depth of Point 1
velocity_of_fluid_at_1 = Absolute Velocity of the Issuing Jet-sqrt(([g]*Depth of Point 2*(Depth of Point 2+Depth of Point 1))/(2*Depth of Point 1))
velocity_of_fluid_at_1 = ((([g]*(Depth of Point 2+Depth of Point 1))/(2*Depth of Point 1))*Height/Celerity of the Wave)+Velocity_of the fluid at 2
velocity_of_fluid_at_1 = (Height*[g]/Celerity of the Wave)+Velocity_of the fluid at 2
velocity_of_fluid_at_1 = ((Absolute Velocity of the Issuing Jet*(Depth of Point 2-Depth of Point 1))+(Velocity_of the fluid at 2*Depth of Point 2))/Depth of Point 1

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