Absolute Velocity for given Normal Thrust Normal to Direction of Jet Calculator

✖Thrust Force acting perpendicular to the job piece.ⓘ Thrust Force [Ft]			+10% -10%
✖Specific Gravity of Fluid is the ratio of the specific weight of a substance to the specific weight of a standard fluid.ⓘ Specific Gravity of Fluid [G]			+10% -10%
✖The Specific Weight of Liquid refers to the weight per unit volume of that substance.ⓘ Specific Weight of Liquid [γ_f]			+10% -10%
✖Cross Sectional Area of Jet is the area of a two-dimensional shape that is obtained when a three-dimensional shape is sliced perpendicular to some specified axis at a point.ⓘ Cross Sectional Area of Jet [A_Jet]			+10% -10%
✖Angle between Jet and Plate is the space between two intersecting lines or surfaces at or close to the point where they meet.ⓘ Angle between Jet and Plate [∠D]			+10% -10%
✖Theta is an angle that can be defined as the figure formed by two rays meeting at a common endpoint.ⓘ Theta [θ]			+10% -10%
✖Velocity of Jet can be described as the movement of the plate in meters per second.ⓘ Velocity of Jet [v]			+10% -10%

✖Absolute Velocity of Issuing Jet is actual velocity of jet used in propeller.ⓘ Absolute Velocity for given Normal Thrust Normal to Direction of Jet [V_absolute]

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Absolute Velocity for given Normal Thrust Normal to Direction of Jet Solution

STEP 0: Pre-Calculation Summary

Formula Used

Absolute Velocity of Issuing Jet = (sqrt((Thrust Force*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet*(Angle between Jet and Plate*(180/pi))*cos(Theta))))+Velocity of Jet
V_absolute = (sqrt((Ft*G)/(γ_f*A_Jet*(∠D*(180/pi))*cos(θ))))+v
This formula uses 1 Constants, 2 Functions, 8 Variables

Constants Used

pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288

Functions Used

cos - Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle., cos(Angle)
sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)

Variables Used

Absolute Velocity of Issuing Jet - (Measured in Meter per Second) - Absolute Velocity of Issuing Jet is actual velocity of jet used in propeller.
Thrust Force - (Measured in Newton) - Thrust Force acting perpendicular to the job piece.
Specific Gravity of Fluid - Specific Gravity of Fluid is the ratio of the specific weight of a substance to the specific weight of a standard fluid.
Specific Weight of Liquid - (Measured in Kilonewton per Cubic Meter) - The Specific Weight of Liquid refers to the weight per unit volume of that substance.
Cross Sectional Area of Jet - (Measured in Square Meter) - Cross Sectional Area of Jet is the area of a two-dimensional shape that is obtained when a three-dimensional shape is sliced perpendicular to some specified axis at a point.
Angle between Jet and Plate - (Measured in Radian) - Angle between Jet and Plate is the space between two intersecting lines or surfaces at or close to the point where they meet.
Theta - (Measured in Radian) - Theta is an angle that can be defined as the figure formed by two rays meeting at a common endpoint.
Velocity of Jet - (Measured in Meter per Second) - Velocity of Jet can be described as the movement of the plate in meters per second.

STEP 1: Convert Input(s) to Base Unit

Thrust Force: 0.5 Kilonewton --> 500 Newton (Check conversion here)
Specific Gravity of Fluid: 10 --> No Conversion Required
Specific Weight of Liquid: 9.81 Kilonewton per Cubic Meter --> 9.81 Kilonewton per Cubic Meter No Conversion Required
Cross Sectional Area of Jet: 1.2 Square Meter --> 1.2 Square Meter No Conversion Required
Angle between Jet and Plate: 11 Degree --> 0.19198621771934 Radian (Check conversion here)
Theta: 30 Degree --> 0.5235987755982 Radian (Check conversion here)
Velocity of Jet: 9.69 Meter per Second --> 9.69 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

V_absolute = (sqrt((Ft*G)/(γ_f*A_Jet*(∠D*(180/pi))*cos(θ))))+v --> (sqrt((500*10)/(9.81*1.2*(0.19198621771934*(180/pi))*cos(0.5235987755982))))+9.69

Evaluating ... ...

V_absolute = 16.367258921457

STEP 3: Convert Result to Output's Unit

16.367258921457 Meter per Second --> No Conversion Required

FINAL ANSWER

16.367258921457 ≈ 16.36726 Meter per Second <-- Absolute Velocity of Issuing Jet

(Calculation completed in 00.010 seconds)

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Created by M Naveen

National Institute of Technology (NIT), Warangal

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National Institute Of Technology (NIT), Hamirpur

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< Absolute Velocity Calculators

Absolute Velocity for given Normal Thrust Normal to Direction of Jet

LaTeX Go Absolute Velocity of Issuing Jet = (sqrt((Thrust Force*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet*(Angle between Jet and Plate*(180/pi))*cos(Theta))))+Velocity of Jet

Absolute Velocity for given Normal Thrust Parallel to Direction of Jet

LaTeX Go Absolute Velocity of Issuing Jet = sqrt((Thrust Force*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet*(Angle between Jet and Plate*(180/pi))^2))+Velocity of Jet

Absolute velocity for dynamic thrust exerted by jet on plate

LaTeX Go Absolute Velocity of Issuing Jet = (sqrt((Fluid Mass*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet*(Angle between Jet and Plate*(180/pi)))))+Velocity of Jet

Absolute Velocity for Mass of Fluid Striking Plate

LaTeX Go Absolute Velocity of Issuing Jet = ((Fluid Mass*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet))+Velocity of Jet

Absolute Velocity for given Normal Thrust Normal to Direction of Jet Formula

LaTeX Go

What is meant by Thrust?

Thrust is a force or a push. When a system pushes or accelerates mass in one direction, there is a thrust (force) just as large in the opposite direction.

How to Calculate Absolute Velocity for given Normal Thrust Normal to Direction of Jet?

Absolute Velocity for given Normal Thrust Normal to Direction of Jet calculator uses Absolute Velocity of Issuing Jet = (sqrt((Thrust Force*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet*(Angle between Jet and Plate*(180/pi))*cos(Theta))))+Velocity of Jet to calculate the Absolute Velocity of Issuing Jet, The Absolute Velocity for given Normal Thrust Normal to Direction of Jet is the rate of change of its position with respect to a frame of reference and is a function of time. Absolute Velocity of Issuing Jet is denoted by V_absolute symbol.

How to calculate Absolute Velocity for given Normal Thrust Normal to Direction of Jet using this online calculator? To use this online calculator for Absolute Velocity for given Normal Thrust Normal to Direction of Jet, enter Thrust Force (Ft), Specific Gravity of Fluid (G), Specific Weight of Liquid (γ_f), Cross Sectional Area of Jet (A_Jet), Angle between Jet and Plate (∠D), Theta (θ) & Velocity of Jet (v) and hit the calculate button. Here is how the Absolute Velocity for given Normal Thrust Normal to Direction of Jet calculation can be explained with given input values -> 16.36726 = (sqrt((500*10)/(9810*1.2*(0.19198621771934*(180/pi))*cos(0.5235987755982))))+9.69.

FAQ

What is Absolute Velocity for given Normal Thrust Normal to Direction of Jet?

The Absolute Velocity for given Normal Thrust Normal to Direction of Jet is the rate of change of its position with respect to a frame of reference and is a function of time and is represented as V_absolute = (sqrt((Ft*G)/(γ_f*A_Jet*(∠D*(180/pi))*cos(θ))))+v or Absolute Velocity of Issuing Jet = (sqrt((Thrust Force*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet*(Angle between Jet and Plate*(180/pi))*cos(Theta))))+Velocity of Jet. Thrust Force acting perpendicular to the job piece, Specific Gravity of Fluid is the ratio of the specific weight of a substance to the specific weight of a standard fluid, The Specific Weight of Liquid refers to the weight per unit volume of that substance, Cross Sectional Area of Jet is the area of a two-dimensional shape that is obtained when a three-dimensional shape is sliced perpendicular to some specified axis at a point, Angle between Jet and Plate is the space between two intersecting lines or surfaces at or close to the point where they meet, Theta is an angle that can be defined as the figure formed by two rays meeting at a common endpoint & Velocity of Jet can be described as the movement of the plate in meters per second.

How to calculate Absolute Velocity for given Normal Thrust Normal to Direction of Jet?

The Absolute Velocity for given Normal Thrust Normal to Direction of Jet is the rate of change of its position with respect to a frame of reference and is a function of time is calculated using Absolute Velocity of Issuing Jet = (sqrt((Thrust Force*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet*(Angle between Jet and Plate*(180/pi))*cos(Theta))))+Velocity of Jet. To calculate Absolute Velocity for given Normal Thrust Normal to Direction of Jet, you need Thrust Force (Ft), Specific Gravity of Fluid (G), Specific Weight of Liquid (γ_f), Cross Sectional Area of Jet (A_Jet), Angle between Jet and Plate (∠D), Theta (θ) & Velocity of Jet (v). With our tool, you need to enter the respective value for Thrust Force, Specific Gravity of Fluid, Specific Weight of Liquid, Cross Sectional Area of Jet, Angle between Jet and Plate, Theta & Velocity of Jet 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 Issuing Jet?

In this formula, Absolute Velocity of Issuing Jet uses Thrust Force, Specific Gravity of Fluid, Specific Weight of Liquid, Cross Sectional Area of Jet, Angle between Jet and Plate, Theta & Velocity of Jet. We can use 3 other way(s) to calculate the same, which is/are as follows -

Absolute Velocity of Issuing Jet = ((Fluid Mass*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet))+Velocity of Jet
Absolute Velocity of Issuing Jet = (sqrt((Fluid Mass*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet*(Angle between Jet and Plate*(180/pi)))))+Velocity of Jet
Absolute Velocity of Issuing Jet = sqrt((Thrust Force*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet*(Angle between Jet and Plate*(180/pi))^2))+Velocity of Jet

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