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## Absolute velocity of the surge moving towards right in postive surges Solution

STEP 0: Pre-Calculation Summary
Formula Used
absolute_velocity = (Velocity_of the fluid at 1*Depth of Point 1-Velocity_of the fluid at 2*Depth of Point 2)/(Depth of Point 2-Depth of Point 1)
V = (V1*h 1-V2*h 2)/(h 2-h 1)
This formula uses 4 Variables
Variables Used
Velocity_of the fluid at 1 - Velocity_of the fluid at 1 is defined as the velocity of the flowing liquid at a point 1 (Measured in Meter per Second)
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)
Velocity_of the fluid at 2 - Velocity_of the fluid at 2 is defined as the velocity of the flowing liquid at point 1. (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)
STEP 1: Convert Input(s) to Base Unit
Velocity_of the fluid at 1: 10 Meter per Second --> 10 Meter per Second No Conversion Required
Depth of Point 1: 10 Meter --> 10 Meter No Conversion Required
Velocity_of the fluid at 2: 5 Meter per Second --> 5 Meter per Second No Conversion Required
Depth of Point 2: 15 Meter --> 15 Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
V = (V1*h 1-V2*h 2)/(h 2-h 1) --> (10*10-5*15)/(15-10)
Evaluating ... ...
V = 5
STEP 3: Convert Result to Output's Unit
5 Meter per Second --> No Conversion Required
5 Meter per Second <-- Absolute Velocity of the Issuing Jet
(Calculation completed in 00.031 seconds)

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

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
Parallel upstream flow components after shock as Mach tends to infinite
parallel_upstream_flow_component = 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
perpedicular_upstream_flow_component = Velocity_of the fluid at 1*((sin(2*Wave angle))/(Specific Heat Ratio-1)) 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
Tangential Momentum of the Fluid Striking the Vanes at the outlet
tangential_momentum = (-Weight of Fluid*Velocity_of the fluid at 1)/ specific gravity of liquid Go
Specific Gravity when Tangential Momentum of the Fluid Striking the Vanes at the Outlet is given
specific_gravity1 = (-Weight of Fluid*Velocity_of the fluid at 1)/ tangential momentum Go
Pressure Difference between two Points in a Liquid
pressure_difference = Specific Weight*(Depth of Point 1-Depth of Point 2) Go
Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given
cross_sectional_area = Discharge/(Density 2*Velocity_of the fluid at 2) Go
Mass Density at Section 2 when flow at Section 1 for a Steady Flow is Given
density_2 = Discharge/(Cross sectional area*Velocity_of the fluid at 2) Go
Cross Sectional Area at Section 1 for a Steady Flow
cross_sectional_area = Discharge/(Density 1*Velocity_of the fluid at 1) Go
Mass Density at Section 1 for a Steady Flow
density_1 = Discharge/(Cross sectional area*Velocity_of the fluid at 1) Go

## < 11 Other formulas that calculate the same Output

Absolute Velocity(V) when Dynamic Thrust Exerted by the Jet on the Plate is given
absolute_velocity = (sqrt((Fluid mass*specific gravity of liquid)/(Specific Weight*Cross sectional area)))+Velocity of Jet Go
Absolute Velocity(V) when Mass of the Fluid Striking the Plate is given
absolute_velocity = ((Fluid mass*specific gravity of liquid)/(Specific Weight*Cross sectional area))+Velocity of Jet Go
Absolute Velocity when Mass of Fluid Striking the Plate is given
absolute_velocity = ((Fluid mass*specific gravity of liquid)/(Specific Weight*Cross sectional area))+Velocity of Jet Go
Jet Velocity when Output Power is Given
absolute_velocity = (Output Power/(Water Density*Rate of flow*flow velocity))+flow velocity Go
Jet Velocity when Power Lost is Given
absolute_velocity = sqrt((Power Loss/(density of fluid*Rate of flow*0.5)))+flow velocity Go
Jet Velocity when Thrust on the Propeller is Given
absolute_velocity = (Thrust force/(Water Density*Rate of flow))+flow velocity Go
Absolute Velocity of the Issuing Jet when Work Done by the Jet on Ship is Given
absolute_velocity = (Work*[g])/(weight of water*Velocity of the Ship) Go
Jet Velocity when Rate of Flow through Propeller is Given
absolute_velocity = (8*Rate of flow/(pi*Diameter^2))-flow velocity Go
Absolute Velocity of the Issuing Jet when Propelling Force is Given
absolute_velocity = [g]*Force/weight of water Go
Absolute Velocity of the Issuing Jet when Relative Velocity is Given
absolute_velocity = Relative Velocity-Velocity of the Ship Go
Jet Velocity when Theoretical Propulsive Efficiency is Given
absolute_velocity = (2/Efficiency-1)*flow velocity Go

### Absolute velocity of the surge moving towards right in postive surges Formula

absolute_velocity = (Velocity_of the fluid at 1*Depth of Point 1-Velocity_of the fluid at 2*Depth of Point 2)/(Depth of Point 2-Depth of Point 1)
V = (V1*h 1-V2*h 2)/(h 2-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 Absolute velocity of the surge moving towards right in postive surges?

Absolute velocity of the surge moving towards right in postive surges calculator uses absolute_velocity = (Velocity_of the fluid at 1*Depth of Point 1-Velocity_of the fluid at 2*Depth of Point 2)/(Depth of Point 2-Depth of Point 1) to calculate the Absolute Velocity of the Issuing Jet, The Absolute velocity of the surge moving towards right in postive surges is defined as velocity of surge irrespective of any medium. Absolute Velocity of the Issuing Jet and is denoted by V symbol.

How to calculate Absolute velocity of the surge moving towards right in postive surges using this online calculator? To use this online calculator for Absolute velocity of the surge moving towards right in postive surges, enter Velocity_of the fluid at 1 (V1), Depth of Point 1 (h 1), Velocity_of the fluid at 2 (V2) and Depth of Point 2 (h 2) and hit the calculate button. Here is how the Absolute velocity of the surge moving towards right in postive surges calculation can be explained with given input values -> 5 = (10*10-5*15)/(15-10).

### FAQ

What is Absolute velocity of the surge moving towards right in postive surges?
The Absolute velocity of the surge moving towards right in postive surges is defined as velocity of surge irrespective of any medium and is represented as V = (V1*h 1-V2*h 2)/(h 2-h 1) or absolute_velocity = (Velocity_of the fluid at 1*Depth of Point 1-Velocity_of the fluid at 2*Depth of Point 2)/(Depth of Point 2-Depth of Point 1). Velocity_of the fluid at 1 is defined as the velocity of the flowing liquid at a point 1, Depth of Point 1 is the depth of point below the free surface in a static mass of liquid, Velocity_of the fluid at 2 is defined as the velocity of the flowing liquid at point 1 and Depth of Point 2 is the depth of point below the free surface in a static mass of liquid.
How to calculate Absolute velocity of the surge moving towards right in postive surges?
The Absolute velocity of the surge moving towards right in postive surges is defined as velocity of surge irrespective of any medium is calculated using absolute_velocity = (Velocity_of the fluid at 1*Depth of Point 1-Velocity_of the fluid at 2*Depth of Point 2)/(Depth of Point 2-Depth of Point 1). To calculate Absolute velocity of the surge moving towards right in postive surges, you need Velocity_of the fluid at 1 (V1), Depth of Point 1 (h 1), Velocity_of the fluid at 2 (V2) and Depth of Point 2 (h 2). With our tool, you need to enter the respective value for Velocity_of the fluid at 1, Depth of Point 1, Velocity_of the fluid at 2 and Depth of Point 2 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 Absolute Velocity of the Issuing Jet?
In this formula, Absolute Velocity of the Issuing Jet uses Velocity_of the fluid at 1, Depth of Point 1, Velocity_of the fluid at 2 and Depth of Point 2. We can use 11 other way(s) to calculate the same, which is/are as follows -
• absolute_velocity = Relative Velocity-Velocity of the Ship
• absolute_velocity = [g]*Force/weight of water
• absolute_velocity = (Work*[g])/(weight of water*Velocity of the Ship)
• absolute_velocity = (Thrust force/(Water Density*Rate of flow))+flow velocity
• absolute_velocity = (8*Rate of flow/(pi*Diameter^2))-flow velocity
• absolute_velocity = (Output Power/(Water Density*Rate of flow*flow velocity))+flow velocity
• absolute_velocity = sqrt((Power Loss/(density of fluid*Rate of flow*0.5)))+flow velocity
• absolute_velocity = (2/Efficiency-1)*flow velocity
• absolute_velocity = ((Fluid mass*specific gravity of liquid)/(Specific Weight*Cross sectional area))+Velocity of Jet
• absolute_velocity = (sqrt((Fluid mass*specific gravity of liquid)/(Specific Weight*Cross sectional area)))+Velocity of Jet
• absolute_velocity = ((Fluid mass*specific gravity of liquid)/(Specific Weight*Cross sectional area))+Velocity of Jet
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