Simplified Pressure Ratio for Blunt Cylinder Blast Wave Solution

STEP 0: Pre-Calculation Summary
Formula Used
Pressure Ratio = 0.0681*Mach Number^2*sqrt(Drag Coefficient)/(Distance from X-Axis/Diameter)
rp = 0.0681*M^2*sqrt(CD)/(y/d)
This formula uses 1 Functions, 5 Variables
Functions Used
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
Pressure Ratio - Pressure Ratio is ratio of final to initial pressure.
Mach Number - Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
Drag Coefficient - 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.
Distance from X-Axis - (Measured in Meter) - Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis.
Diameter - (Measured in Meter) - Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.
STEP 1: Convert Input(s) to Base Unit
Mach Number: 5.5 --> No Conversion Required
Drag Coefficient: 0.19866 --> No Conversion Required
Distance from X-Axis: 2.2 Meter --> 2.2 Meter No Conversion Required
Diameter: 2.425 Meter --> 2.425 Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
rp = 0.0681*M^2*sqrt(CD)/(y/d) --> 0.0681*5.5^2*sqrt(0.19866)/(2.2/2.425)
Evaluating ... ...
rp = 1.01208448803177
STEP 3: Convert Result to Output's Unit
1.01208448803177 --> No Conversion Required
FINAL ANSWER
1.01208448803177 1.012084 <-- Pressure Ratio
(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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PSG College of Technology (PSGCT), Coimbatore
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Cylindrical Blast Wave Calculators

Modified Pressure Equation for Cylindrical Blast Wave
​ LaTeX ​ Go Modified Pressure = [BoltZ]*Freestream Density*sqrt(pi/8)*Diameter*sqrt(Drag Coefficient)*(Freestream Velocity^2)/Distance from X-Axis
Boltzmann Constant for Cylindrical Blast Wave
​ LaTeX ​ Go Boltzmann Constant = (Specific Heat Ratio^(2*(Specific Heat Ratio-1)/(2-Specific Heat Ratio)))/(2^((4-Specific Heat Ratio)/(2-Specific Heat Ratio)))
Pressure for Cylindrical Blast Wave
​ LaTeX ​ Go Pressure for Blast Wave = Boltzmann Constant*Freestream Density*((Energy for Blast Wave/Freestream Density)^(1/2))/(Time Required for Blast Wave)
Radial Coordinate of Cylindrical Blast Wave
​ LaTeX ​ Go Radial Coordinate = (Energy for Blast Wave/Freestream Density)^(1/4)*Time Required for Blast Wave^(1/2)

Simplified Pressure Ratio for Blunt Cylinder Blast Wave Formula

​LaTeX ​Go
Pressure Ratio = 0.0681*Mach Number^2*sqrt(Drag Coefficient)/(Distance from X-Axis/Diameter)
rp = 0.0681*M^2*sqrt(CD)/(y/d)

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 Simplified Pressure Ratio for Blunt Cylinder Blast Wave?

Simplified Pressure Ratio for Blunt Cylinder Blast Wave calculator uses Pressure Ratio = 0.0681*Mach Number^2*sqrt(Drag Coefficient)/(Distance from X-Axis/Diameter) to calculate the Pressure Ratio, Simplified Pressure Ratio for Blunt Cylinder Blast Wave formula is defined as a dimensionless quantity that characterizes the pressure ratio of a blast wave in a blunt cylinder, providing a crucial parameter in the analysis of blast wave propagation and its effects on structures and environments. Pressure Ratio is denoted by rp symbol.

How to calculate Simplified Pressure Ratio for Blunt Cylinder Blast Wave using this online calculator? To use this online calculator for Simplified Pressure Ratio for Blunt Cylinder Blast Wave, enter Mach Number (M), Drag Coefficient (CD), Distance from X-Axis (y) & Diameter (d) and hit the calculate button. Here is how the Simplified Pressure Ratio for Blunt Cylinder Blast Wave calculation can be explained with given input values -> 1.012084 = 0.0681*5.5^2*sqrt(0.19866)/(2.2/2.425).

FAQ

What is Simplified Pressure Ratio for Blunt Cylinder Blast Wave?
Simplified Pressure Ratio for Blunt Cylinder Blast Wave formula is defined as a dimensionless quantity that characterizes the pressure ratio of a blast wave in a blunt cylinder, providing a crucial parameter in the analysis of blast wave propagation and its effects on structures and environments and is represented as rp = 0.0681*M^2*sqrt(CD)/(y/d) or Pressure Ratio = 0.0681*Mach Number^2*sqrt(Drag Coefficient)/(Distance from X-Axis/Diameter). Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound, 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, Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis & Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.
How to calculate Simplified Pressure Ratio for Blunt Cylinder Blast Wave?
Simplified Pressure Ratio for Blunt Cylinder Blast Wave formula is defined as a dimensionless quantity that characterizes the pressure ratio of a blast wave in a blunt cylinder, providing a crucial parameter in the analysis of blast wave propagation and its effects on structures and environments is calculated using Pressure Ratio = 0.0681*Mach Number^2*sqrt(Drag Coefficient)/(Distance from X-Axis/Diameter). To calculate Simplified Pressure Ratio for Blunt Cylinder Blast Wave, you need Mach Number (M), Drag Coefficient (CD), Distance from X-Axis (y) & Diameter (d). With our tool, you need to enter the respective value for Mach Number, Drag Coefficient, Distance from X-Axis & Diameter 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 Ratio?
In this formula, Pressure Ratio uses Mach Number, Drag Coefficient, Distance from X-Axis & Diameter. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Pressure Ratio = 0.127*Mach Number^2*Drag Coefficient^(2/3)*(Distance from X-Axis/Diameter)^(-2/3)
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