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Cross Sectional Area for given Normal Thrust Normal to Direction of Jet Formula

GoCross Section Area for Mass of Fluid Striking Plate Formula

GoCross Sectional Area for given Dynamic Thrust Exerted by Jet on Plate Formula

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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. Check FAQs

A Jet = \frac{Ft \cdot G}{γ f \cdot {(V absolute - v)}^{2} \cdot (∠D \cdot (\frac{180}{π})) \cdot \cos (θ)}

A_Jet - Cross Sectional Area of Jet?Ft - Thrust Force?G - Specific Gravity of Fluid?γ_f - Specific Weight of Liquid?V_absolute - Absolute Velocity of Issuing Jet?v - Velocity of Jet?∠D - Angle between Jet and Plate?θ - Theta?π - Archimedes' constant?

Cross Sectional Area for given Normal Thrust Normal to Direction of Jet Example

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Here is how the Cross Sectional Area for given Normal Thrust Normal to Direction of Jet equation looks like with Values.

Here is how the Cross Sectional Area for given Normal Thrust Normal to Direction of Jet equation looks like with Units.

Here is how the Cross Sectional Area for given Normal Thrust Normal to Direction of Jet equation looks like.

0.3183 = \frac{0.5 \cdot 10}{9.81 \cdot {(10.1 - 9.69)}^{2} \cdot (11 \cdot (\frac{180}{3.1416})) \cdot \cos (30)}

0.3183m² = \frac{0.5kN \cdot 10}{9.81kN/m³ \cdot {(10.1m/s - 9.69m/s)}^{2} \cdot (11° \cdot (\frac{180}{3.1416})) \cdot \cos (30°)}

0.3183 = \frac{0.5 \cdot 10}{9.81 \cdot {(10.1 - 9.69)}^{2} \cdot (11 \cdot (\frac{180}{3.1416})) \cdot \cos (30)}

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Cross Sectional Area for given Normal Thrust Normal to Direction of Jet Solution

Follow our step by step solution on how to calculate Cross Sectional Area for given Normal Thrust Normal to Direction of Jet?

FIRST Step Consider the formula

A Jet = \frac{Ft \cdot G}{γ f \cdot {(V absolute - v)}^{2} \cdot (∠D \cdot (\frac{180}{π})) \cdot \cos (θ)}

Next Step Substitute values of Variables

∴

A Jet = \frac{0.5kN \cdot 10}{9.81kN/m³ \cdot {(10.1m/s - 9.69m/s)}^{2} \cdot (11° \cdot (\frac{180}{π})) \cdot \cos (30°)}

Next Step Substitute values of Constants

∴

A Jet = \frac{0.5kN \cdot 10}{9.81kN/m³ \cdot {(10.1m/s - 9.69m/s)}^{2} \cdot (11° \cdot (\frac{180}{3.1416})) \cdot \cos (30°)}

Next Step Convert Units

∴

A Jet = \frac{500N \cdot 10}{9810N/m³ \cdot {(10.1m/s - 9.69m/s)}^{2} \cdot (0.192rad \cdot (\frac{180}{3.1416})) \cdot \cos (0.5236rad)}

Next Step Prepare to Evaluate

∴

A Jet = \frac{500 \cdot 10}{9810 \cdot {(10.1 - 9.69)}^{2} \cdot (0.192 \cdot (\frac{180}{3.1416})) \cdot \cos (0.5236)}

Next Step Evaluate

∴

A Jet = 0.318280452379613m²

LAST Step Rounding Answer

∴

A Jet = 0.3183m²

Cross Sectional Area for given Normal Thrust Normal to Direction of Jet Formula Elements

Variables

Constants

Functions

Cross Sectional Area of Jet

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.

Symbol: A_Jet

Measurement: AreaUnit: m²

Note: Value should be greater than 0.

Formulas to find Cross Sectional Area of Jet

Thrust Force

Thrust Force acting perpendicular to the job piece.

Symbol: Ft

Measurement: ForceUnit: kN

Note: Value should be greater than 0.

Formulas to find Thrust Force

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.

Symbol: G

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Specific Gravity of Fluid

Specific Weight of Liquid

The Specific Weight of Liquid refers to the weight per unit volume of that substance.

Symbol: γ_f

Measurement: Specific WeightUnit: kN/m³

Note: Value should be greater than 0.

Formulas to find Specific Weight of Liquid

Absolute Velocity of Issuing Jet

Absolute Velocity of Issuing Jet is actual velocity of jet used in propeller.

Symbol: V_absolute

Measurement: SpeedUnit: m/s

Note: Value can be positive or negative.

Formulas to find Absolute Velocity of Issuing Jet

Velocity of Jet

Velocity of Jet can be described as the movement of the plate in meters per second.

Symbol: v

Measurement: SpeedUnit: m/s

Note: Value can be positive or negative.

Formulas to find Velocity of Jet

Angle between Jet and Plate

Angle between Jet and Plate is the space between two intersecting lines or surfaces at or close to the point where they meet.

Symbol: ∠D

Measurement: AngleUnit: °

Note: Value can be positive or negative.

Formulas to find Angle between Jet and Plate

Theta

Theta is an angle that can be defined as the figure formed by two rays meeting at a common endpoint.

Symbol: θ

Measurement: AngleUnit: °

Note: Value can be positive or negative.

Formulas to find Theta

Archimedes' constant

Archimedes' constant is a mathematical constant that represents the ratio of the circumference of a circle to its diameter.

Symbol: π

Value: 3.14159265358979323846264338327950288

cos

Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle.

Syntax: cos(Angle)

Other Formulas to find Cross Sectional Area of Jet

Go Cross Section Area for Mass of Fluid Striking Plate

A Jet = \frac{m f \cdot G}{γ f \cdot (V absolute - v)}

Go Cross Sectional Area for given Dynamic Thrust Exerted by Jet on Plate

A Jet = \frac{m f \cdot G}{γ f \cdot (∠D \cdot (\frac{180}{π})) \cdot {(V absolute - v jet)}^{2}}

How to Evaluate Cross Sectional Area for given Normal Thrust Normal to Direction of Jet?

Cross Sectional Area for given Normal Thrust Normal to Direction of Jet evaluator uses Cross Sectional Area of Jet = (Thrust Force*Specific Gravity of Fluid)/(Specific Weight of Liquid*(Absolute Velocity of Issuing Jet-Velocity of Jet)^2*(Angle between Jet and Plate*(180/pi))*cos(Theta)) to evaluate the Cross Sectional Area of Jet, The Cross Sectional Area for given Normal Thrust Normal to Direction of Jet is the area of a two-dimensional shape that is obtained when a three-dimensional object - such as a cylinder. Cross Sectional Area of Jet is denoted by A_Jet symbol.

How to evaluate Cross Sectional Area for given Normal Thrust Normal to Direction of Jet using this online evaluator? To use this online evaluator for Cross Sectional Area for given Normal Thrust Normal to Direction of Jet, enter Thrust Force (Ft), Specific Gravity of Fluid (G), Specific Weight of Liquid (γ_f), Absolute Velocity of Issuing Jet (V_absolute), Velocity of Jet (v), Angle between Jet and Plate (∠D) & Theta (θ) and hit the calculate button.

FAQs on Cross Sectional Area for given Normal Thrust Normal to Direction of Jet

What is the formula to find Cross Sectional Area for given Normal Thrust Normal to Direction of Jet?

The formula of Cross Sectional Area for given Normal Thrust Normal to Direction of Jet is expressed as Cross Sectional Area of Jet = (Thrust Force*Specific Gravity of Fluid)/(Specific Weight of Liquid*(Absolute Velocity of Issuing Jet-Velocity of Jet)^2*(Angle between Jet and Plate*(180/pi))*cos(Theta)). Here is an example- 0.556742 = (500*10)/(9810*(10.1-9.69)^2*(0.19198621771934*(180/pi))*cos(0.5235987755982)).

How to calculate Cross Sectional Area for given Normal Thrust Normal to Direction of Jet?

With Thrust Force (Ft), Specific Gravity of Fluid (G), Specific Weight of Liquid (γ_f), Absolute Velocity of Issuing Jet (V_absolute), Velocity of Jet (v), Angle between Jet and Plate (∠D) & Theta (θ) we can find Cross Sectional Area for given Normal Thrust Normal to Direction of Jet using the formula - Cross Sectional Area of Jet = (Thrust Force*Specific Gravity of Fluid)/(Specific Weight of Liquid*(Absolute Velocity of Issuing Jet-Velocity of Jet)^2*(Angle between Jet and Plate*(180/pi))*cos(Theta)). This formula also uses Archimedes' constant and Cosine (cos) function(s).

What are the other ways to Calculate Cross Sectional Area of Jet?

Here are the different ways to Calculate Cross Sectional Area of Jet-

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

Can the Cross Sectional Area for given Normal Thrust Normal to Direction of Jet be negative?

No, the Cross Sectional Area for given Normal Thrust Normal to Direction of Jet, measured in Area cannot be negative.

Which unit is used to measure Cross Sectional Area for given Normal Thrust Normal to Direction of Jet?

Cross Sectional Area for given Normal Thrust Normal to Direction of Jet is usually measured using the Square Meter[m²] for Area. Square Kilometer[m²], Square Centimeter[m²], Square Millimeter[m²] are the few other units in which Cross Sectional Area for given Normal Thrust Normal to Direction of Jet can be measured.

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Cross Sectional Area for given Normal Thrust Normal to Direction of Jet Formula

​GoCross Section Area for Mass of Fluid Striking Plate Formula

​GoCross Sectional Area for given Dynamic Thrust Exerted by Jet on Plate Formula

Cross Sectional Area for given Normal Thrust Normal to Direction of Jet Example

Cross Sectional Area for given Normal Thrust Normal to Direction of Jet Solution

Cross Sectional Area for given Normal Thrust Normal to Direction of Jet Formula Elements

Other Formulas to find Cross Sectional Area of Jet

How to Evaluate Cross Sectional Area for given Normal Thrust Normal to Direction of Jet?

FAQs on Cross Sectional Area for given Normal Thrust Normal to Direction of Jet

Variable Name

GoCross Section Area for Mass of Fluid Striking Plate Formula

GoCross Sectional Area for given Dynamic Thrust Exerted by Jet on Plate Formula