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

✖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.ⓘ Distance from X-Axis [y]			+10% -10%
✖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.ⓘ Length of Shuttle [l]			+10% -10%
✖The Angle of Attack is the angle between the direction of motion of an object and its longitudinal axis in blast wave theory.ⓘ Angle of Attack [α]			+10% -10%

✖The Pressure Coefficient is a dimensionless quantity used to describe the ratio of dynamic pressure to static pressure in a blast wave.ⓘ Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack [C_p]

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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 - The Pressure Coefficient is a dimensionless quantity used to describe the ratio of dynamic pressure to static pressure in a blast wave.
Distance from X-Axis - (Measured in Meter) - 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.
Length of Shuttle - (Measured in Meter) - 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.
Angle of Attack - (Measured in Radian) - The Angle of Attack is the angle between the direction of motion of an object and its longitudinal axis in blast wave theory.

STEP 1: Convert Input(s) to Base Unit

Distance from X-Axis: 2200 Millimeter --> 2.2 Meter (Check conversion here)
Length of Shuttle: 87.5912409 Millimeter --> 0.0875912409 Meter (Check conversion here)
Angle of Attack: 39.5 Degree --> 0.689405054537631 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/(2.2/0.0875912409)+2*(sin(0.689405054537631))^2

Evaluating ... ...

C_p = 0.809736459168806

STEP 3: Convert Result to Output's Unit

0.809736459168806 --> No Conversion Required

FINAL ANSWER

0.809736459168806 ≈ 0.809736 <-- Pressure Coefficient

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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Indian Institute of Technology (IIT), Bombay

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< Blast Wave Part Theory Calculators

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

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

Pressure Coefficient for Blunt-Nosed Cylinder

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

Pressure Coefficient for Blunt-Nosed Plate

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

Pressure Coefficient Combined with Blast Wave for Shuttle

LaTeX 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

LaTeX Go

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?

Pressure Coefficient is a dimensionless number used in fluid dynamics to describe the relative pressure throughout a flow field.

What is a Blast Wave?

A blast wave is a high-pressure wave that propagates outward from an explosion that consists of a leading shock front of compressed gases, followed by a blast wind of negative pressure that can suck items back towards the explosion’s center. This wave travels at supersonic speeds and can cause significant damage due to the rapid rise and subsequent drop in pressure.

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, 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 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 -> 0.792634 = 0.0137/(2.2/0.0875912409)+2*(sin(0.689405054537631))^2.

FAQ

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

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

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 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 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 3 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)

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