Modified pressure equation for cylindrical blast wave Calculator

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✖Freestream density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitudeⓘ Freestream density [ρ_∞]			+10% -10%
✖Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.ⓘ Diameter [d]			+10% -10%
✖Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or waterⓘ Drag Coefficient [C_D]			+10% -10%
✖The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the airⓘ Freestream Velocity [V_∞]			+10% -10%
✖Distance from X-axis is defined as the distance from the point where stress is to be computed to XX axis.ⓘ Distance from X-axis [y]			+10% -10%

✖The pressure is defined as the physical force exerted on an object. It is symbolized by P.ⓘ Modified pressure equation for cylindrical blast wave [P]

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Modified pressure equation for cylindrical blast wave

Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 300+ more calculators!

Shikha Maurya

Indian Institute of Technology (IIT), Bombay

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

Heat Loss due to Pipe

Heat Loss due to Pipe=(Force*Length*Fluid Velocity^2)/(2*Diameter *Acceleration Due To Gravity) GO

Reynolds Number for Circular Tubes

Reynolds Number=Density*Fluid Velocity*Diameter /Dynamic viscosity GO

Perimeter of a Semicircle when circumference of circle is given

Perimeter=(Circumference of Circle/2)+Diameter GO

Diameter of circumscribing sphere when diameter and height of circumscribed cylinder is known

Diameter of Sphere=sqrt(Diameter ^2+Height^2) GO

Cutting Speed

Cutting Speed=pi*Diameter *Angular Speed GO

Area of a Circle when diameter is given

Area of Circle=(pi/4)*Diameter ^2 GO

Perimeter of a quarter circle when diameter is given

Perimeter=Diameter *((pi/4)+1) GO

Perimeter of a Semicircle when diameter is given

Perimeter=Diameter *((pi/2)+1) GO

Area of a quarter circle when diameter is given

Area=(pi*(Diameter )^2)/16 GO

Area of a Semicircle when diameter is given

Area=(pi*(Diameter )^2)/8 GO

Radius of a circle when diameter is given

Radius=Diameter /2 GO

< 11 Other formulas that calculate the same Output

New pressure after the shock formation for compression wave

Pressure=density ahead of shock*(1+((Specific Heat Ratio-1)/2)*(Normal velocity/Old speed of sound))^(2*Specific Heat Ratio/(Specific Heat Ratio-Time)) GO

Pressure for the cylindrical blast wave

Pressure=Boltzmann constant 1*Freestream density*((Energy/Freestream density)^(1/2))/(Time) GO

formula For creation pressure for the planar blast wave

Pressure=[BoltZ]*Freestream density*((Energy/Freestream density)^(2/3))*(Time)^(-2/3) GO

Pressure when Resultant is Outside Middle Third

Pressure=2*Total downward force on soil/(3*middle third distance) GO

Pressure of the liquid entering the motor

Pressure=Theoretical torque/Theoretical volumetric displacement GO

Pressure

Pressure=(1/3)*Density of Gas*(Root mean square velocity)^2 GO

Pressure when density and height are given

Pressure=Density*Acceleration Due To Gravity*Height GO

Pressure during retraction

Pressure=Force/(Area of piston-Area of piston rod) GO

Pressure in Excess of Atmospheric Pressure

Pressure=(specific weight of liquid)*(Height) GO

Pressure exerted

Pressure=Force/Area of piston GO

Pressure when force and area are given

Pressure=Force/Area GO

Modified pressure equation for cylindrical blast wave Formula

Pressure=[BoltZ]*Freestream density*(sqrt(pi/8))*Diameter *(sqrt(Drag Coefficient))*(Freestream Velocity^2/Distance from X-axis)
P=[BoltZ]*ρ∞*(sqrt(pi/8))*d*(sqrt(CD))*(V∞^2/y)

More formulas

Pressure for the cylindrical blast wave GO

Boltzmann constant for cylindrical blast wave GO

formula For creation pressure for the planar blast wave GO

Radial coordinate of cylindrical blast wave GO

Radial coordinate for the planar blast wave, GO

Energy for the blast wave GO

Time required for the blast wave GO

Pressure ratio for blunt cylinder blast wave GO

Simplified pressure ratio for blunt cylinder blast wave GO

Modified Radial coordinate equation for cylindrical blast wave GO

Modified Energy for the cylindrical blast wave GO

Coefficient of drag equation using energy released from blast wave GO

Pressure ratio for blunt slab blast wave GO

Radial coordinate of blunt slab blast wave GO

Blunt-nosed flat plate pressure ratio (first approximation) GO

What is boltzmann constant?

The Boltzmann constant (kB or k) is the proportionality factor that relates the average relative kinetic energy of particles in a gas with the thermodynamic temperature of the gas

How to Calculate Modified pressure equation for cylindrical blast wave?

Modified pressure equation for cylindrical blast wave calculator uses Pressure=[BoltZ]*Freestream density*(sqrt(pi/8))*Diameter *(sqrt(Drag Coefficient))*(Freestream Velocity^2/Distance from X-axis) to calculate the Pressure, The Modified pressure equation for cylindrical blast wave formula is defined as the interrelation between the Boltzmann constant, drag coeff, freestream velocity, base dia and distance x from tip. Pressure and is denoted by P symbol.

How to calculate Modified pressure equation for cylindrical blast wave using this online calculator? To use this online calculator for Modified pressure equation for cylindrical blast wave, enter Freestream density (ρ_∞), Diameter (d), Drag Coefficient (C_D), Freestream Velocity (V_∞) and Distance from X-axis (y) and hit the calculate button. Here is how the Modified pressure equation for cylindrical blast wave calculation can be explained with given input values -> 1.060E-15 = [BoltZ]*1.225*(sqrt(pi/8))*10*(sqrt(100))*(100^2/0.01).

FAQ

What is Modified pressure equation for cylindrical blast wave?

The Modified pressure equation for cylindrical blast wave formula is defined as the interrelation between the Boltzmann constant, drag coeff, freestream velocity, base dia and distance x from tip and is represented as P=[BoltZ]*ρ_∞*(sqrt(pi/8))*d*(sqrt(C_D))*(V_∞^2/y) or Pressure=[BoltZ]*Freestream density*(sqrt(pi/8))*Diameter *(sqrt(Drag Coefficient))*(Freestream Velocity^2/Distance from X-axis). Freestream density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitude, Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere, Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water, The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air and Distance from X-axis is defined as the distance from the point where stress is to be computed to XX axis.

How to calculate Modified pressure equation for cylindrical blast wave?

The Modified pressure equation for cylindrical blast wave formula is defined as the interrelation between the Boltzmann constant, drag coeff, freestream velocity, base dia and distance x from tip is calculated using Pressure=[BoltZ]*Freestream density*(sqrt(pi/8))*Diameter *(sqrt(Drag Coefficient))*(Freestream Velocity^2/Distance from X-axis). To calculate Modified pressure equation for cylindrical blast wave, you need Freestream density (ρ_∞), Diameter (d), Drag Coefficient (C_D), Freestream Velocity (V_∞) and Distance from X-axis (y). With our tool, you need to enter the respective value for Freestream density, Diameter , Drag Coefficient, Freestream Velocity and Distance from X-axis 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 Pressure?

In this formula, Pressure uses Freestream density, Diameter , Drag Coefficient, Freestream Velocity and Distance from X-axis. We can use 11 other way(s) to calculate the same, which is/are as follows -

Pressure=Force/Area
Pressure=Density*Acceleration Due To Gravity*Height
Pressure=(specific weight of liquid)*(Height)
Pressure=(1/3)*Density of Gas*(Root mean square velocity)^2
Pressure=2*Total downward force on soil/(3*middle third distance)
Pressure=Theoretical torque/Theoretical volumetric displacement
Pressure=Force/Area of piston
Pressure=Force/(Area of piston-Area of piston rod)
Pressure=Boltzmann constant 1*Freestream density*((Energy/Freestream density)^(1/2))/(Time)
Pressure=[BoltZ]*Freestream density*((Energy/Freestream density)^(2/3))*(Time)^(-2/3)
Pressure=density ahead of shock*(1+((Specific Heat Ratio-1)/2)*(Normal velocity/Old speed of sound))^(2*Specific Heat Ratio/(Specific Heat Ratio-Time))

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