Pressure Coefficient Combined with Blast Wave for Shuttle Calculator

✖Distance from Nose Tip to Required Base Diameter, used for studying the leading edge of the hypersonic vehicles.ⓘ Distance from Nose Tip to Required Base Diameter [x_d]			+10% -10%
✖Length of Shuttle variable is used for studying the coefficient of pressure.ⓘ Length of Shuttle [l]			+10% -10%

✖Pressure coefficient defines the value of local pressure at a point in terms of free stream pressure and dynamic pressure.ⓘ 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 - Pressure coefficient defines the value of local pressure at a point in terms of free stream pressure and dynamic pressure.
Distance from Nose Tip to Required Base Diameter - (Measured in Meter) - Distance from Nose Tip to Required Base Diameter, used for studying the leading edge of the hypersonic vehicles.
Length of Shuttle - (Measured in Meter) - Length of Shuttle variable is used for studying the coefficient of pressure.

STEP 1: Convert Input(s) to Base Unit

Distance from Nose Tip to Required Base Diameter: 1.2 Meter --> 1.2 Meter No Conversion Required
Length of Shuttle: 500 Millimeter --> 0.5 Meter (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_p = 0.0137/(x_d/l) --> 0.0137/(1.2/0.5)

Evaluating ... ...

C_p = 0.00570833333333333

STEP 3: Convert Result to Output's Unit

0.00570833333333333 --> No Conversion Required

FINAL ANSWER

0.00570833333333333 ≈ 0.005708 <-- 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

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

Pressure Coefficient for Blunt-Nosed Cylinder

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

Pressure Coefficient for Blunt-Nosed Plate

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

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

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?

The pressure coefficient is a dimensionless number which describes the relative pressures throughout a flow field in fluid dynamics.

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 -> 0.835366 = 0.0137/(1.2/0.5).

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). Distance from Nose Tip to Required Base Diameter, used for studying the leading edge of the hypersonic vehicles & Length of Shuttle variable is used for studying the coefficient of pressure.

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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