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Pressure Coefficient Combined with Blast Wave for Shuttle 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 = \frac{0.0137}{\frac{x d}{l}}

C_p - Pressure Coefficient?x_d - 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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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.

0.0057 = \frac{0.0137}{\frac{1.2}{500}}

0.0057 = \frac{0.0137}{\frac{1.2m}{500mm}}

0.0057 = \frac{0.0137}{\frac{1.2}{500}}

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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

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

Next Step Substitute values of Variables

∴

C p = \frac{0.0137}{\frac{1.2m}{500mm}}

Next Step Convert Units

∴

C p = \frac{0.0137}{\frac{1.2m}{0.5m}}

Next Step Prepare to Evaluate

∴

C p = \frac{0.0137}{\frac{1.2}{0.5}}

Next Step Evaluate

∴

C p = 0.00570833333333333

LAST Step Rounding Answer

∴

C p = 0.0057

Pressure Coefficient Combined with Blast Wave for Shuttle 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

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: m

Note: Value can be positive or negative.

Formulas to find Distance from Nose Tip to Required Base Diameter

Length of Shuttle

Length of Shuttle variable is used for studying the coefficient of pressure.

Symbol: l

Measurement: LengthUnit: mm

Note: Value should be greater than 0.

Formulas to find Length of Shuttle

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 for Blunt-Nosed Cylinder

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

Go Pressure Coefficient for Blast Wave Theory

C p = \frac{2}{Y \cdot M^{2}} \cdot (r p - 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, The Pressure coefficient combined with blast wave for shuttle formula is defined as the inverse of the ratio of the distance from the tip of shuttle to the length of the shuttle. Pressure Coefficient is denoted by C_p 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 (x_d) & 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- 0.835366 = 0.0137/(1.2/0.5).

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

With Distance from Nose Tip to Required Base Diameter (x_d) & 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))^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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