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Force exerted by body on supersonic plane Solution

STEP 0: Pre-Calculation Summary
Formula Used
force = (Density of Fluid*(Change in length^2)*(Velocity of body^2))*((Viscosity of fluid)/(Density of Fluid*Velocity of body*Change in length))*((Bulk Modulus)/(Density of Fluid*Velocity of body^2))
F = (ρFluid*(ΔL^2)*(v^2))*((μ)/(ρFluid*v*ΔL))*((K)/(ρFluid*v^2))
This formula uses 5 Variables
Variables Used
Density of Fluid - Density of Fluid is defined as the mass of fluid per unit volume of the said fluid. (Measured in Kilogram per Meter³)
Change in length - Change in length is the changed length of the body after it has been subjected to stress. (Measured in Meter)
Velocity of body - Velocity of body is the velocity at which the body is moving. (Measured in Meter per Second)
Viscosity of fluid - The Viscosity of fluid is a measure of its resistance to deformation at a given rate. (Measured in Newton Second per Meter²)
Bulk Modulus - The Bulk Modulus is defined as the ratio of the infinitesimal pressure increase to the resulting relative decrease of the volume. (Measured in Newton per Square Meter)
STEP 1: Convert Input(s) to Base Unit
Density of Fluid: 10 Kilogram per Meter³ --> 10 Kilogram per Meter³ No Conversion Required
Change in length: 25 Meter --> 25 Meter No Conversion Required
Velocity of body: 48 Meter per Second --> 48 Meter per Second No Conversion Required
Viscosity of fluid: 10 Newton Second per Meter² --> 10 Pascal Second (Check conversion here)
Bulk Modulus: 1000 Newton per Square Meter --> 1000 Pascal (Check conversion here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
F = (ρFluid*(ΔL^2)*(v^2))*((μ)/(ρFluid*v*ΔL))*((K)/(ρFluid*v^2)) --> (10*(25^2)*(48^2))*((10)/(10*48*25))*((1000)/(10*48^2))
Evaluating ... ...
F = 520.833333333333
STEP 3: Convert Result to Output's Unit
520.833333333333 Newton --> No Conversion Required
FINAL ANSWER
520.833333333333 Newton <-- Force
(Calculation completed in 00.016 seconds)

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Location of stagnation points for a rotating cylinder in a uniform flow field
angle_at_stagnation_point = -asin(Circulation/(4*pi*Freestream Velocity*Cylinder Radius)) Go
Skin friction drag from total drag force on a sphere
skin_friction_drag_froce = 2*pi*Viscosity of fluid*Diameter of sphere*Flow Velocity Go
Area of the body for lift force in body moving on fluid
reference_area = Lift force/(Lift Coefficient*0.5*Density of Fluid*(Velocity^2)) Go
Pressure drag from total drag force on a sphere
pressure_drag_force = pi*Viscosity of fluid*Diameter of sphere*Flow Velocity Go
Drag force for a body moving in a fluid of certain density
drag_force = Coefficient of drag*Area of Surface*Density*(Velocity^2)/2 Go
Lift force on a cylinder for circulation
lift_force = Density*Length of Cylinder*Circulation*Freestream Velocity Go
Total drag force on a sphere
drag_force = 3*pi*Viscosity of fluid*Diameter of sphere*Flow Velocity Go
Length of the cylinder for lift force on a cylinder
length_cylinder = Lift force/(Density*Circulation*Freestream Velocity) Go
Lift force for a body moving in a fluid of certain density
lift_force_ = Lift Coefficient*Reference Area*Density*(Velocity^2)/2 Go
Radius of cylinder for lift coefficient in a rotating cylinder with circulation
radius_of_cylinder = Circulation/(Lift Coefficient*Freestream Velocity) Go

Force exerted by body on supersonic plane Formula

force = (Density of Fluid*(Change in length^2)*(Velocity of body^2))*((Viscosity of fluid)/(Density of Fluid*Velocity of body*Change in length))*((Bulk Modulus)/(Density of Fluid*Velocity of body^2))
F = (ρFluid*(ΔL^2)*(v^2))*((μ)/(ρFluid*v*ΔL))*((K)/(ρFluid*v^2))

What is super sonic speed ?

Supersonic speed is the speed of an object that exceeds the speed of sound. For objects traveling in dry air of a temperature of 20 °C at sea level, this speed is approximately 343.2 m/s. Speeds greater than five times the speed of sound are often referred to as hypersonic.

What is force with example?

Force is defined as an external cause that changes or tends to change the state of the body once applied, if the body is in motion it comes to rest and if at rest then will come to motion. Example: Pushing or pulling a door by applying force.

How to Calculate Force exerted by body on supersonic plane?

Force exerted by body on supersonic plane calculator uses force = (Density of Fluid*(Change in length^2)*(Velocity of body^2))*((Viscosity of fluid)/(Density of Fluid*Velocity of body*Change in length))*((Bulk Modulus)/(Density of Fluid*Velocity of body^2)) to calculate the Force, The Force exerted by body on supersonic plane formula is defined as a push or pull upon an object resulting from the object's interaction with another object. Force is denoted by F symbol.

How to calculate Force exerted by body on supersonic plane using this online calculator? To use this online calculator for Force exerted by body on supersonic plane, enter Density of Fluid Fluid), Change in length (ΔL), Velocity of body (v), Viscosity of fluid (μ) & Bulk Modulus (K) and hit the calculate button. Here is how the Force exerted by body on supersonic plane calculation can be explained with given input values -> 520.8333 = (10*(25^2)*(48^2))*((10)/(10*48*25))*((1000)/(10*48^2)).

FAQ

What is Force exerted by body on supersonic plane?
The Force exerted by body on supersonic plane formula is defined as a push or pull upon an object resulting from the object's interaction with another object and is represented as F = (ρFluid*(ΔL^2)*(v^2))*((μ)/(ρFluid*v*ΔL))*((K)/(ρFluid*v^2)) or force = (Density of Fluid*(Change in length^2)*(Velocity of body^2))*((Viscosity of fluid)/(Density of Fluid*Velocity of body*Change in length))*((Bulk Modulus)/(Density of Fluid*Velocity of body^2)). Density of Fluid is defined as the mass of fluid per unit volume of the said fluid, Change in length is the changed length of the body after it has been subjected to stress, Velocity of body is the velocity at which the body is moving, The Viscosity of fluid is a measure of its resistance to deformation at a given rate & The Bulk Modulus is defined as the ratio of the infinitesimal pressure increase to the resulting relative decrease of the volume.
How to calculate Force exerted by body on supersonic plane?
The Force exerted by body on supersonic plane formula is defined as a push or pull upon an object resulting from the object's interaction with another object is calculated using force = (Density of Fluid*(Change in length^2)*(Velocity of body^2))*((Viscosity of fluid)/(Density of Fluid*Velocity of body*Change in length))*((Bulk Modulus)/(Density of Fluid*Velocity of body^2)). To calculate Force exerted by body on supersonic plane, you need Density of Fluid Fluid), Change in length (ΔL), Velocity of body (v), Viscosity of fluid (μ) & Bulk Modulus (K). With our tool, you need to enter the respective value for Density of Fluid, Change in length, Velocity of body, Viscosity of fluid & Bulk Modulus 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 Force?
In this formula, Force uses Density of Fluid, Change in length, Velocity of body, Viscosity of fluid & Bulk Modulus. We can use 10 other way(s) to calculate the same, which is/are as follows -
  • drag_force = Coefficient of drag*Area of Surface*Density*(Velocity^2)/2
  • lift_force_ = Lift Coefficient*Reference Area*Density*(Velocity^2)/2
  • reference_area = Lift force/(Lift Coefficient*0.5*Density of Fluid*(Velocity^2))
  • drag_force = 3*pi*Viscosity of fluid*Diameter of sphere*Flow Velocity
  • skin_friction_drag_froce = 2*pi*Viscosity of fluid*Diameter of sphere*Flow Velocity
  • pressure_drag_force = pi*Viscosity of fluid*Diameter of sphere*Flow Velocity
  • lift_force = Density*Length of Cylinder*Circulation*Freestream Velocity
  • length_cylinder = Lift force/(Density*Circulation*Freestream Velocity)
  • radius_of_cylinder = Circulation/(Lift Coefficient*Freestream Velocity)
  • angle_at_stagnation_point = -asin(Circulation/(4*pi*Freestream Velocity*Cylinder Radius))
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