Dynamic Thrust Exerted on Plate by Jet Solution

STEP 0: Pre-Calculation Summary
Formula Used
Thrust Force = (Specific Weight of Liquid*Cross Sectional Area of Jet*(Absolute Velocity of Issuing Jet-Velocity of Jet)^2)/Specific Gravity of Fluid
Ft = (γf*AJet*(Vabsolute-v)^2)/G
This formula uses 6 Variables
Variables Used
Thrust Force - (Measured in Newton) - Thrust Force acting perpendicular to the job piece.
Specific Weight of Liquid - (Measured in Newton 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.
Absolute Velocity of Issuing Jet - (Measured in Meter per Second) - Absolute Velocity of Issuing Jet is actual velocity of jet used in propeller.
Velocity of Jet - (Measured in Meter per Second) - Velocity of Jet can be described as the movement of the plate in meters per second.
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.
STEP 1: Convert Input(s) to Base Unit
Specific Weight of Liquid: 9.81 Kilonewton per Cubic Meter --> 9810 Newton per Cubic Meter (Check conversion ​here)
Cross Sectional Area of Jet: 1.2 Square Meter --> 1.2 Square Meter No Conversion Required
Absolute Velocity of Issuing Jet: 10.1 Meter per Second --> 10.1 Meter per Second No Conversion Required
Velocity of Jet: 9.69 Meter per Second --> 9.69 Meter per Second No Conversion Required
Specific Gravity of Fluid: 10 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Ft = (γf*AJet*(Vabsolute-v)^2)/G --> (9810*1.2*(10.1-9.69)^2)/10
Evaluating ... ...
Ft = 197.88732
STEP 3: Convert Result to Output's Unit
197.88732 Newton -->0.19788732 Kilonewton (Check conversion ​here)
FINAL ANSWER
0.19788732 0.197887 Kilonewton <-- Thrust Force
(Calculation completed in 00.004 seconds)

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Flat Plate Normal to the Jet Calculators

Velocity of jet given dynamic thrust exerted by jet on plate
​ LaTeX ​ Go Velocity of Jet = -(sqrt((Fluid Mass*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet))-Absolute Velocity of Issuing Jet)
Absolute Velocity given 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)))+Velocity of Jet
Velocity of jet for mass of fluid striking plate
​ LaTeX ​ Go Velocity of Jet = -(((Fluid Mass*Specific Gravity of Fluid)/(Specific Weight of Liquid*Cross Sectional Area of Jet))-Absolute Velocity of Issuing Jet)
Dynamic Thrust Exerted on Plate by Jet
​ LaTeX ​ Go Thrust Force = (Specific Weight of Liquid*Cross Sectional Area of Jet*(Absolute Velocity of Issuing Jet-Velocity of Jet)^2)/Specific Gravity of Fluid

Dynamic Thrust Exerted on Plate by Jet Formula

​LaTeX ​Go
Thrust Force = (Specific Weight of Liquid*Cross Sectional Area of Jet*(Absolute Velocity of Issuing Jet-Velocity of Jet)^2)/Specific Gravity of Fluid
Ft = (γf*AJet*(Vabsolute-v)^2)/G

What is meant by Velocity?

The Velocity of an object is the rate of change of its position with respect to a frame of reference, and is a function of time.

How to Calculate Dynamic Thrust Exerted on Plate by Jet?

Dynamic Thrust Exerted on Plate by Jet calculator uses Thrust Force = (Specific Weight of Liquid*Cross Sectional Area of Jet*(Absolute Velocity of Issuing Jet-Velocity of Jet)^2)/Specific Gravity of Fluid to calculate the Thrust Force, Dynamic Thrust Exerted on Plate by Jet is defined as the force exerted by the jet in the direction of parallel to the plate. Thrust Force is denoted by Ft symbol.

How to calculate Dynamic Thrust Exerted on Plate by Jet using this online calculator? To use this online calculator for Dynamic Thrust Exerted on Plate by Jet, enter Specific Weight of Liquid f), Cross Sectional Area of Jet (AJet), Absolute Velocity of Issuing Jet (Vabsolute), Velocity of Jet (v) & Specific Gravity of Fluid (G) and hit the calculate button. Here is how the Dynamic Thrust Exerted on Plate by Jet calculation can be explained with given input values -> 0.000113 = (9810*1.2*(10.1-9.69)^2)/10.

FAQ

What is Dynamic Thrust Exerted on Plate by Jet?
Dynamic Thrust Exerted on Plate by Jet is defined as the force exerted by the jet in the direction of parallel to the plate and is represented as Ft = (γf*AJet*(Vabsolute-v)^2)/G or Thrust Force = (Specific Weight of Liquid*Cross Sectional Area of Jet*(Absolute Velocity of Issuing Jet-Velocity of Jet)^2)/Specific Gravity of 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, Absolute Velocity of Issuing Jet is actual velocity of jet used in propeller, Velocity of Jet can be described as the movement of the plate in meters per second & Specific Gravity of Fluid is the ratio of the specific weight of a substance to the specific weight of a standard fluid.
How to calculate Dynamic Thrust Exerted on Plate by Jet?
Dynamic Thrust Exerted on Plate by Jet is defined as the force exerted by the jet in the direction of parallel to the plate is calculated using Thrust Force = (Specific Weight of Liquid*Cross Sectional Area of Jet*(Absolute Velocity of Issuing Jet-Velocity of Jet)^2)/Specific Gravity of Fluid. To calculate Dynamic Thrust Exerted on Plate by Jet, you need Specific Weight of Liquid f), Cross Sectional Area of Jet (AJet), Absolute Velocity of Issuing Jet (Vabsolute), Velocity of Jet (v) & Specific Gravity of Fluid (G). With our tool, you need to enter the respective value for Specific Weight of Liquid, Cross Sectional Area of Jet, Absolute Velocity of Issuing Jet, Velocity of Jet & Specific Gravity of Fluid and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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