FormulaDen.com

Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health

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

Fx Copy

LaTeX Copy

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{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

With values

With units

Only example

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.

0.0751 = \frac{0.0137}{\frac{2200}{500}} + 2 \cdot {(\sin (10.94))}^{2}

0.0751 = \frac{0.0137}{\frac{2200mm}{500mm}} + 2 \cdot {(\sin (10.94°))}^{2}

0.0751 = \frac{0.0137}{\frac{2200}{500}} + 2 \cdot {(\sin (10.94))}^{2}

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Engineering » Category

Mechanical » Category

Fluid Mechanics » fx Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack

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}{500mm}} + 2 \cdot {(\sin (10.94°))}^{2}

Next Step Convert Units

∴

C p = \frac{0.0137}{\frac{2.2m}{0.5m}} + 2 \cdot {(\sin (0.1909rad))}^{2}

Next Step Prepare to Evaluate

∴

C p = \frac{0.0137}{\frac{2.2}{0.5}} + 2 \cdot {(\sin (0.1909))}^{2}

Next Step Evaluate

∴

C p = 0.0751472416968372

LAST Step Rounding Answer

∴

C p = 0.0751

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

Variables

Functions

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 X-Axis

Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis.

Symbol: y

Measurement: LengthUnit: mm

Note: Value can be positive or negative.

Formulas to find Distance from X-Axis

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

Angle of Attack

Angle of attack is the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving.

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)

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

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