Pressure Coefficient Combined with Blast Wave for Shuttle Calculator

✖The Distance from Nose Tip to Required Base Diameter is the length from the nose tip to the base diameter of a blast wave in an explosive event.ⓘ Distance from Nose Tip to Required Base Diameter [x_d]			+10% -10%
✖The Length of Shuttle is the distance from the center of the explosive to the point where the blast wave is being measured or observed.ⓘ Length of Shuttle [l]			+10% -10%

✖The Pressure Coefficient is a dimensionless quantity used to describe the ratio of dynamic pressure to static pressure in a blast wave.ⓘ Pressure Coefficient Combined with Blast Wave for Shuttle [C_p]

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Pressure Coefficient Combined with Blast Wave for Shuttle Solution

STEP 0: Pre-Calculation Summary

Formula Used

Pressure Coefficient = 0.0137/(Distance from Nose Tip to Required Base Diameter/Length of Shuttle)
C_p = 0.0137/(x_d/l)
This formula uses 3 Variables

Variables Used

Pressure Coefficient - The Pressure Coefficient is a dimensionless quantity used to describe the ratio of dynamic pressure to static pressure in a blast wave.
Distance from Nose Tip to Required Base Diameter - (Measured in Meter) - The Distance from Nose Tip to Required Base Diameter is the length from the nose tip to the base diameter of a blast wave in an explosive event.
Length of Shuttle - (Measured in Meter) - The Length of Shuttle is the distance from the center of the explosive to the point where the blast wave is being measured or observed.

STEP 1: Convert Input(s) to Base Unit

Distance from Nose Tip to Required Base Diameter: 1.5 Millimeter --> 0.0015 Meter (Check conversion here)
Length of Shuttle: 87.5912409 Millimeter --> 0.0875912409 Meter (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_p = 0.0137/(x_d/l) --> 0.0137/(0.0015/0.0875912409)

Evaluating ... ...

C_p = 0.80000000022

STEP 3: Convert Result to Output's Unit

0.80000000022 --> No Conversion Required

FINAL ANSWER

0.80000000022 ≈ 0.8 <-- Pressure Coefficient

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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Indian Institute of Technology (IIT), Bombay

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< Blast Wave Part Theory Calculators

Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack

LaTeX Go Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2

Pressure Coefficient for Blunt-Nosed Cylinder

LaTeX Go Pressure Coefficient = 0.096*(Drag Coefficient^(1/2))/(Distance from Nose Tip to Required Base Diameter/Diameter)

Pressure Coefficient for Blunt-Nosed Plate

LaTeX Go Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3))

Pressure Coefficient Combined with Blast Wave for Shuttle

LaTeX Go Pressure Coefficient = 0.0137/(Distance from Nose Tip to Required Base Diameter/Length of Shuttle)

Pressure Coefficient Combined with Blast Wave for Shuttle Formula

LaTeX Go

Pressure Coefficient = 0.0137/(Distance from Nose Tip to Required Base Diameter/Length of Shuttle)
C_p = 0.0137/(x_d/l)

What is Pressure Coefficient?

Pressure Coefficient is a dimensionless number used in fluid dynamics to describe the relative pressure throughout a flow field.

What is a Blast Wave?

A blast wave is a high-pressure wave that propagates outward from an explosion that consists of a leading shock front of compressed gases, followed by a blast wind of negative pressure that can suck items back towards the explosion’s center. This wave travels at supersonic speeds and can cause significant damage due to the rapid rise and subsequent drop in pressure.

How to Calculate Pressure Coefficient Combined with Blast Wave for Shuttle?

Pressure Coefficient Combined with Blast Wave for Shuttle calculator uses Pressure Coefficient = 0.0137/(Distance from Nose Tip to Required Base Diameter/Length of Shuttle) to calculate the Pressure Coefficient, Pressure Coefficient Combined with Blast Wave for Shuttle formula is defined as a dimensionless parameter that characterizes the pressure distribution around a shuttle during a blast wave event, providing a crucial factor in understanding the aerodynamic and structural responses of the shuttle to such events. Pressure Coefficient is denoted by C_p symbol.

How to calculate Pressure Coefficient Combined with Blast Wave for Shuttle using this online calculator? To use this online calculator for Pressure Coefficient Combined with Blast Wave for Shuttle, enter Distance from Nose Tip to Required Base Diameter (x_d) & Length of Shuttle (l) and hit the calculate button. Here is how the Pressure Coefficient Combined with Blast Wave for Shuttle calculation can be explained with given input values -> 4.566667 = 0.0137/(0.0015/0.0875912409).

FAQ

What is Pressure Coefficient Combined with Blast Wave for Shuttle?

Pressure Coefficient Combined with Blast Wave for Shuttle formula is defined as a dimensionless parameter that characterizes the pressure distribution around a shuttle during a blast wave event, providing a crucial factor in understanding the aerodynamic and structural responses of the shuttle to such events and is represented as C_p = 0.0137/(x_d/l) or Pressure Coefficient = 0.0137/(Distance from Nose Tip to Required Base Diameter/Length of Shuttle). The Distance from Nose Tip to Required Base Diameter is the length from the nose tip to the base diameter of a blast wave in an explosive event & The Length of Shuttle is the distance from the center of the explosive to the point where the blast wave is being measured or observed.

How to calculate Pressure Coefficient Combined with Blast Wave for Shuttle?

Pressure Coefficient Combined with Blast Wave for Shuttle formula is defined as a dimensionless parameter that characterizes the pressure distribution around a shuttle during a blast wave event, providing a crucial factor in understanding the aerodynamic and structural responses of the shuttle to such events is calculated using Pressure Coefficient = 0.0137/(Distance from Nose Tip to Required Base Diameter/Length of Shuttle). To calculate Pressure Coefficient Combined with Blast Wave for Shuttle, you need Distance from Nose Tip to Required Base Diameter (x_d) & Length of Shuttle (l). With our tool, you need to enter the respective value for Distance from Nose Tip to Required Base Diameter & Length of Shuttle 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 Coefficient?

In this formula, Pressure Coefficient uses Distance from Nose Tip to Required Base Diameter & Length of Shuttle. We can use 3 other way(s) to calculate the same, which is/are as follows -

Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2
Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3))
Pressure Coefficient = 0.096*(Drag Coefficient^(1/2))/(Distance from Nose Tip to Required Base Diameter/Diameter)

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