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Pressure Coefficient for Blunt-Nosed Cylinder Formula

GoPressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack Formula

GoPressure Coefficient for Blunt-Nosed Plate Formula

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Pressure coefficient defines the value of local pressure at a point in terms of free stream pressure and dynamic pressure. Check FAQs

C p = 0.096 \cdot \frac{{C d}^{\frac{1}{2}}}{\frac{x d}{d}}

C_p - Pressure Coefficient?C_d - Drag Coefficient?x_d - Distance from Nose Tip to Required Base Diameter?d - Diameter?

Pressure Coefficient for Blunt-Nosed Cylinder Example

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Here is how the Pressure Coefficient for Blunt-Nosed Cylinder equation looks like with Values.

Here is how the Pressure Coefficient for Blunt-Nosed Cylinder equation looks like with Units.

Here is how the Pressure Coefficient for Blunt-Nosed Cylinder equation looks like.

0.0052 = 0.096 \cdot \frac{{2.4}^{\frac{1}{2}}}{\frac{1200}{42}}

0.0052 = 0.096 \cdot \frac{{2.4}^{\frac{1}{2}}}{\frac{1200mm}{42mm}}

0.0052 = 0.096 \cdot \frac{{2.4}^{\frac{1}{2}}}{\frac{1200}{42}}

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Pressure Coefficient for Blunt-Nosed Cylinder Solution

Follow our step by step solution on how to calculate Pressure Coefficient for Blunt-Nosed Cylinder?

FIRST Step Consider the formula

C p = 0.096 \cdot \frac{{C d}^{\frac{1}{2}}}{\frac{x d}{d}}

Next Step Substitute values of Variables

∴

C p = 0.096 \cdot \frac{{2.4}^{\frac{1}{2}}}{\frac{1200mm}{42mm}}

Next Step Convert Units

∴

C p = 0.096 \cdot \frac{{2.4}^{\frac{1}{2}}}{\frac{1.2m}{0.042m}}

Next Step Prepare to Evaluate

∴

C p = 0.096 \cdot \frac{{2.4}^{\frac{1}{2}}}{\frac{1.2}{0.042}}

Next Step Evaluate

∴

C p = 0.00520528961730277

LAST Step Rounding Answer

∴

C p = 0.0052

Pressure Coefficient for Blunt-Nosed Cylinder Formula Elements

Variables

Pressure Coefficient

Pressure coefficient defines the value of local pressure at a point in terms of free stream pressure and dynamic pressure.

Symbol: C_p

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Pressure Coefficient

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.

Symbol: C_d

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Drag Coefficient

Distance from Nose Tip to Required Base Diameter

Distance from Nose Tip to Required Base Diameter, used for studying the leading edge of the hypersonic vehicles.

Symbol: x_d

Measurement: LengthUnit: mm

Note: Value can be positive or negative.

Formulas to find Distance from Nose Tip to Required Base Diameter

Diameter

Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.

Symbol: d

Measurement: LengthUnit: mm

Note: Value should be greater than 0.

Formulas to find Diameter

Other Formulas to find Pressure Coefficient

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

C p = \frac{0.0137}{\frac{y}{l}} + 2 \cdot {(\sin (α))}^{2}

Go Pressure Coefficient for Blunt-Nosed Plate

C p = 0.173 \cdot \frac{{C d}^{\frac{2}{3}}}{{(\frac{x}{d 1})}^{\frac{2}{3}}}

Go Pressure Coefficient Combined with Blast Wave for Shuttle

C p = \frac{0.0137}{\frac{x d}{l}}

Go Pressure Coefficient for Blast Wave Theory

C p = \frac{2}{Y \cdot M^{2}} \cdot (r p - 1)

How to Evaluate Pressure Coefficient for Blunt-Nosed Cylinder?

Pressure Coefficient for Blunt-Nosed Cylinder evaluator uses Pressure Coefficient = 0.096*(Drag Coefficient^(1/2))/(Distance from Nose Tip to Required Base Diameter/Diameter) to evaluate the Pressure Coefficient, Pressure Coefficient for Blunt-Nosed Cylinder formula is defined as a dimensionless quantity that characterizes the pressure distribution around a blunt-nosed cylinder in a blast wave, providing a crucial parameter in the analysis of blast wave propagation and its effects on structures. Pressure Coefficient is denoted by C_p symbol.

How to evaluate Pressure Coefficient for Blunt-Nosed Cylinder using this online evaluator? To use this online evaluator for Pressure Coefficient for Blunt-Nosed Cylinder, enter Drag Coefficient (C_d), Distance from Nose Tip to Required Base Diameter (x_d) & Diameter (d) and hit the calculate button.

FAQs on Pressure Coefficient for Blunt-Nosed Cylinder

What is the formula to find Pressure Coefficient for Blunt-Nosed Cylinder?

The formula of Pressure Coefficient for Blunt-Nosed Cylinder is expressed as Pressure Coefficient = 0.096*(Drag Coefficient^(1/2))/(Distance from Nose Tip to Required Base Diameter/Diameter). Here is an example- 0.798337 = 0.096*(2.4^(1/2))/(0.0015/0.00806872).

How to calculate Pressure Coefficient for Blunt-Nosed Cylinder?

With Drag Coefficient (C_d), Distance from Nose Tip to Required Base Diameter (x_d) & Diameter (d) we can find Pressure Coefficient for Blunt-Nosed Cylinder using the formula - Pressure Coefficient = 0.096*(Drag Coefficient^(1/2))/(Distance from Nose Tip to Required Base Diameter/Diameter).

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

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Pressure Coefficient for Blunt-Nosed Cylinder Formula

​GoPressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack Formula

​GoPressure Coefficient for Blunt-Nosed Plate Formula

Pressure Coefficient for Blunt-Nosed Cylinder Example

Pressure Coefficient for Blunt-Nosed Cylinder Solution

Pressure Coefficient for Blunt-Nosed Cylinder Formula Elements

Other Formulas to find Pressure Coefficient

How to Evaluate Pressure Coefficient for Blunt-Nosed Cylinder?

FAQs on Pressure Coefficient for Blunt-Nosed Cylinder

Variable Name

GoPressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack Formula

GoPressure Coefficient for Blunt-Nosed Plate Formula