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

✖Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis.ⓘ Distance from X-Axis [y]			+10% -10%
✖Length of Shuttle variable is used for studying the coefficient of pressure.ⓘ Length of Shuttle [l]			+10% -10%
✖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.ⓘ Angle of Attack [α]			+10% -10%

✖Pressure coefficient defines the value of local pressure at a point in terms of free stream pressure and dynamic pressure.ⓘ Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack [C_p]

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Formula

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

Formula

`"C"_{"p"} = 0.0137/("y"/"l")+2*(sin("α"))^2`

Example

`"0.075147"=0.0137/("2200mm"/"500mm")+2*(sin("10.94°"))^2`

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

STEP 0: Pre-Calculation Summary

Formula Used

Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2
C_p = 0.0137/(y/l)+2*(sin(α))^2
This formula uses 1 Functions, 4 Variables

Functions Used

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., sin(Angle)

Variables Used

Pressure Coefficient - Pressure coefficient defines the value of local pressure at a point in terms of free stream pressure and dynamic pressure.
Distance from X-Axis - (Measured in Meter) - Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis.
Length of Shuttle - (Measured in Meter) - Length of Shuttle variable is used for studying the coefficient of pressure.
Angle of Attack - (Measured in Radian) - 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.

STEP 1: Convert Input(s) to Base Unit

Distance from X-Axis: 2200 Millimeter --> 2.2 Meter (Check conversion here)
Length of Shuttle: 500 Millimeter --> 0.5 Meter (Check conversion here)
Angle of Attack: 10.94 Degree --> 0.190939020168144 Radian (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_p = 0.0137/(y/l)+2*(sin(α))^2 --> 0.0137/(2.2/0.5)+2*(sin(0.190939020168144))^2

Evaluating ... ...

C_p = 0.0751472416968372

STEP 3: Convert Result to Output's Unit

0.0751472416968372 --> No Conversion Required

FINAL ANSWER

0.0751472416968372 ≈ 0.075147 <-- Pressure Coefficient

(Calculation completed in 00.004 seconds)

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Home » Engineering » Mechanical » Fluid Mechanics » Hypersonic Flow » Blast Wave Part Theory » Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack

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< 6 Blast Wave Part Theory Calculators

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

Go Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2

Pressure Coefficient for Blunt-Nosed Cylinder

Go Pressure Coefficient = 0.096*(Drag Coefficient^(1/2))/(Distance from Nose Tip to Required Base Diameter/Diameter)

Pressure Coefficient for Blunt-Nosed Plate

Go Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3))

Pressure Coefficient for Blast Wave Theory

Go Pressure Coefficient = 2/(Specific Heat Ratio*Mach Number^2)*(Pressure Ratio-1)

Pressure Coefficient for Blast Wave Theory at Very High Values of Mach

Go Pressure Coefficient = 2/(Specific Heat Ratio*Mach Number^2)*Pressure Ratio

Pressure Coefficient Combined with Blast Wave for Shuttle

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

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

Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2
C_p = 0.0137/(y/l)+2*(sin(α))^2

What is pressure coefficient?

The pressure coefficient is a dimensionless number which describes the relative pressures throughout a flow field in fluid dynamics.

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

Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack calculator uses Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2 to calculate the Pressure Coefficient, The Pressure coefficient combined with blast wave for shuttle at angle of attack formula is defined as the inverse of ratio of the distance from the tip of shuttle to the length of the shuttle plus double the square of angle of attack. Pressure Coefficient is denoted by C_p symbol.

How to calculate Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack using this online calculator? To use this online calculator 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. Here is how the Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack calculation can be explained with given input values -> 0.075147 = 0.0137/(2.2/0.5)+2*(sin(0.190939020168144))^2.

FAQ

What is Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack?

The Pressure coefficient combined with blast wave for shuttle at angle of attack formula is defined as the inverse of ratio of the distance from the tip of shuttle to the length of the shuttle plus double the square of angle of attack and is represented as C_p = 0.0137/(y/l)+2*(sin(α))^2 or Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2. Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis, Length of Shuttle variable is used for studying the coefficient of pressure & 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.

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

The Pressure coefficient combined with blast wave for shuttle at angle of attack formula is defined as the inverse of ratio of the distance from the tip of shuttle to the length of the shuttle plus double the square of angle of attack is calculated using Pressure Coefficient = 0.0137/(Distance from X-Axis/Length of Shuttle)+2*(sin(Angle of Attack))^2. To calculate Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack, you need Distance from X-Axis (y), Length of Shuttle (l) & Angle of Attack (α). With our tool, you need to enter the respective value for Distance from X-Axis, Length of Shuttle & Angle of Attack and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Pressure Coefficient?

In this formula, Pressure Coefficient uses Distance from X-Axis, Length of Shuttle & Angle of Attack. We can use 5 other way(s) to calculate the same, which is/are as follows -

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)
Pressure Coefficient = 2/(Specific Heat Ratio*Mach Number^2)*(Pressure Ratio-1)
Pressure Coefficient = 2/(Specific Heat Ratio*Mach Number^2)*Pressure Ratio

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