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The Pressure Coefficient is a dimensionless quantity used to describe the ratio of dynamic pressure to static pressure in a blast wave. Check FAQs
Cp=0.0137xdl
Cp - Pressure Coefficient?xd - Distance from Nose Tip to Required Base Diameter?l - Length of Shuttle?

Pressure Coefficient Combined with Blast Wave for Shuttle Example

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With units
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Here is how the Pressure Coefficient Combined with Blast Wave for Shuttle equation looks like with Values.

Here is how the Pressure Coefficient Combined with Blast Wave for Shuttle equation looks like with Units.

Here is how the Pressure Coefficient Combined with Blast Wave for Shuttle equation looks like.

0.8Edit=0.01371.5Edit87.5912Edit
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Pressure Coefficient Combined with Blast Wave for Shuttle Solution

Follow our step by step solution on how to calculate Pressure Coefficient Combined with Blast Wave for Shuttle?

FIRST Step Consider the formula
Cp=0.0137xdl
Next Step Substitute values of Variables
Cp=0.01371.5mm87.5912mm
Next Step Convert Units
Cp=0.01370.0015m0.0876m
Next Step Prepare to Evaluate
Cp=0.01370.00150.0876
Next Step Evaluate
Cp=0.80000000022
LAST Step Rounding Answer
Cp=0.8

Pressure Coefficient Combined with Blast Wave for Shuttle Formula Elements

Variables
Pressure Coefficient
The Pressure Coefficient is a dimensionless quantity used to describe the ratio of dynamic pressure to static pressure in a blast wave.
Symbol: Cp
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Distance from Nose Tip to Required Base Diameter
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.
Symbol: xd
Measurement: LengthUnit: mm
Note: Value can be positive or negative.
Length of Shuttle
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.
Symbol: l
Measurement: LengthUnit: mm
Note: Value should be greater than 0.

Other Formulas to find Pressure Coefficient

​Go Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack
Cp=0.0137yl+2(sin(α))2
​Go Pressure Coefficient for Blunt-Nosed Plate
Cp=0.173Cd23(xd1)23
​Go Pressure Coefficient for Blunt-Nosed Cylinder
Cp=0.096Cd12xdd
​Go Pressure Coefficient for Blast Wave Theory
Cp=2YM2(rp-1)

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

Pressure Coefficient Combined with Blast Wave for Shuttle evaluator uses Pressure Coefficient = 0.0137/(Distance from Nose Tip to Required Base Diameter/Length of Shuttle) to evaluate 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 Cp symbol.

How to evaluate Pressure Coefficient Combined with Blast Wave for Shuttle using this online evaluator? To use this online evaluator for Pressure Coefficient Combined with Blast Wave for Shuttle, enter Distance from Nose Tip to Required Base Diameter (xd) & Length of Shuttle (l) and hit the calculate button.

FAQs on Pressure Coefficient Combined with Blast Wave for Shuttle

What is the formula to find Pressure Coefficient Combined with Blast Wave for Shuttle?
The formula of Pressure Coefficient Combined with Blast Wave for Shuttle is expressed as Pressure Coefficient = 0.0137/(Distance from Nose Tip to Required Base Diameter/Length of Shuttle). Here is an example- 4.566667 = 0.0137/(0.0015/0.0875912409).
How to calculate Pressure Coefficient Combined with Blast Wave for Shuttle?
With Distance from Nose Tip to Required Base Diameter (xd) & Length of Shuttle (l) we can find Pressure Coefficient Combined with Blast Wave for Shuttle using the formula - Pressure Coefficient = 0.0137/(Distance from Nose Tip to Required Base Diameter/Length of Shuttle).
What are the other ways to Calculate Pressure Coefficient?
Here are the different ways to Calculate Pressure Coefficient-
  • Pressure Coefficient=0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2OpenImg
  • Pressure Coefficient=0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3))OpenImg
  • Pressure Coefficient=0.096*(Drag Coefficient^(1/2))/(Distance from Nose Tip to Required Base Diameter/Diameter)OpenImg
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