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

GoPressure Coefficient for Blunt-Nosed Plate Formula

GoPressure Coefficient for Blunt-Nosed Cylinder Formula

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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

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

C_p - Pressure Coefficient?y - Distance from X-Axis?l - Length of Shuttle?α - Angle of Attack?

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

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Here is how the Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack equation looks like with Values.

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

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

0.8097 = \frac{0.0137}{\frac{2200}{87.5912}} + 2 \cdot {(\sin (39.5))}^{2}

0.8097 = \frac{0.0137}{\frac{2200mm}{87.5912mm}} + 2 \cdot {(\sin (39.5°))}^{2}

0.8097 = \frac{0.0137}{\frac{2200}{87.5912}} + 2 \cdot {(\sin (39.5))}^{2}

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

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

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

C p = \frac{0.0137}{\frac{2200mm}{87.5912mm}} + 2 \cdot {(\sin (39.5°))}^{2}

Next Step Convert Units

∴

C p = \frac{0.0137}{\frac{2.2m}{0.0876m}} + 2 \cdot {(\sin (0.6894rad))}^{2}

Next Step Prepare to Evaluate

∴

C p = \frac{0.0137}{\frac{2.2}{0.0876}} + 2 \cdot {(\sin (0.6894))}^{2}

Next Step Evaluate

∴

C p = 0.809736459168806

LAST Step Rounding Answer

∴

C p = 0.8097

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

Variables

Functions

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: C_p

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Pressure Coefficient

Distance from X-Axis

The Distance from X-Axis is the perpendicular distance of a point from the x-axis in the blast wave theory, used to analyze shockwave propagation.

Symbol: y

Measurement: LengthUnit: mm

Note: Value can be positive or negative.

Formulas to find Distance from X-Axis

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.

Formulas to find Length of Shuttle

Angle of Attack

The Angle of Attack is the angle between the direction of motion of an object and its longitudinal axis in blast wave theory.

Symbol: α

Measurement: AngleUnit: °

Note: Value can be positive or negative.

Formulas to find Angle of Attack

sin

Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse.

Syntax: sin(Angle)

Other Formulas to find Pressure Coefficient

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 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 Combined with Blast Wave for Shuttle at Angle of Attack?

Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack evaluator uses Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2 to evaluate the Pressure Coefficient, Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack formula is defined as a dimensionless quantity that characterizes the pressure distribution around a shuttle during ascent or re-entry into the Earth's atmosphere, influenced by the angle of attack and blast wave effects. Pressure Coefficient is denoted by C_p symbol.

How to evaluate Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack using this online evaluator? To use this online evaluator for Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack, enter Distance from X-Axis (y), Length of Shuttle (l) & Angle of Attack (α) and hit the calculate button.

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

What is the formula to find Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack?

The formula of Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack is expressed as Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2. Here is an example- 0.792634 = 0.0137/(2.2/0.0875912409)+2*(sin(0.689405054537631))^2.

How to calculate Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack?

With Distance from X-Axis (y), Length of Shuttle (l) & Angle of Attack (α) we can find Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack using the formula - Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2. This formula also uses Sine (sin) function(s).

What are the other ways to Calculate Pressure Coefficient?

Here are the different ways to Calculate Pressure Coefficient-

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

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

​GoPressure Coefficient for Blunt-Nosed Plate Formula

​GoPressure Coefficient for Blunt-Nosed Cylinder Formula

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

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

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

Other Formulas to find Pressure Coefficient

How to Evaluate Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack?

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

Variable Name

GoPressure Coefficient for Blunt-Nosed Plate Formula

GoPressure Coefficient for Blunt-Nosed Cylinder Formula