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Pressure Coefficient for Blunt-Nosed Plate Formula

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

GoPressure Coefficient for Blunt-Nosed Cylinder 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 = 0.173 \cdot \frac{{C d}^{\frac{2}{3}}}{{(\frac{x}{d 1})}^{\frac{2}{3}}}

C_p - Pressure Coefficient?C_d - Drag Coefficient?x - Distance from Y-Axis?d₁ - Diameter 1?

Pressure Coefficient for Blunt-Nosed Plate Example

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Here is how the Pressure Coefficient for Blunt-Nosed Plate equation looks like with Values.

Here is how the Pressure Coefficient for Blunt-Nosed Plate equation looks like with Units.

Here is how the Pressure Coefficient for Blunt-Nosed Plate equation looks like.

0.6034 = 0.173 \cdot \frac{{2.4}^{\frac{2}{3}}}{{(\frac{7}{19})}^{\frac{2}{3}}}

0.6034 = 0.173 \cdot \frac{{2.4}^{\frac{2}{3}}}{{(\frac{7mm}{19mm})}^{\frac{2}{3}}}

0.6034 = 0.173 \cdot \frac{{2.4}^{\frac{2}{3}}}{{(\frac{7}{19})}^{\frac{2}{3}}}

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Pressure Coefficient for Blunt-Nosed Plate Solution

Follow our step by step solution on how to calculate Pressure Coefficient for Blunt-Nosed Plate?

FIRST Step Consider the formula

C p = 0.173 \cdot \frac{{C d}^{\frac{2}{3}}}{{(\frac{x}{d 1})}^{\frac{2}{3}}}

Next Step Substitute values of Variables

∴

C p = 0.173 \cdot \frac{{2.4}^{\frac{2}{3}}}{{(\frac{7mm}{19mm})}^{\frac{2}{3}}}

Next Step Convert Units

∴

C p = 0.173 \cdot \frac{{2.4}^{\frac{2}{3}}}{{(\frac{0.007m}{0.019m})}^{\frac{2}{3}}}

Next Step Prepare to Evaluate

∴

C p = 0.173 \cdot \frac{{2.4}^{\frac{2}{3}}}{{(\frac{0.007}{0.019})}^{\frac{2}{3}}}

Next Step Evaluate

∴

C p = 0.603425934337034

LAST Step Rounding Answer

∴

C p = 0.6034

Pressure Coefficient for Blunt-Nosed Plate 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

Drag Coefficient

Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.

Symbol: C_d

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Drag Coefficient

Distance from Y-Axis

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

Symbol: x

Measurement: LengthUnit: mm

Note: Value can be positive or negative.

Formulas to find Distance from Y-Axis

Diameter 1

The Diameter 1 is denoted by the symbol d1.

Symbol: d₁

Measurement: LengthUnit: mm

Note: Value can be positive or negative.

Formulas to find Diameter 1

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 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 for Blunt-Nosed Plate?

Pressure Coefficient for Blunt-Nosed Plate evaluator uses Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3)) to evaluate the Pressure Coefficient, The Pressure coefficient for Blunt-nosed plate formula is defined as the inter relation between drag coefficient, distance from the tip of the blunt nose and base diameter, since its an axis symmetric body the distance is taken along the x axis, where tip of the body is origin. Pressure Coefficient is denoted by C_p symbol.

How to evaluate Pressure Coefficient for Blunt-Nosed Plate using this online evaluator? To use this online evaluator for Pressure Coefficient for Blunt-Nosed Plate, enter Drag Coefficient (C_d), Distance from Y-Axis (x) & Diameter 1 (d₁) and hit the calculate button.

FAQs on Pressure Coefficient for Blunt-Nosed Plate

What is the formula to find Pressure Coefficient for Blunt-Nosed Plate?

The formula of Pressure Coefficient for Blunt-Nosed Plate is expressed as Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3)). Here is an example- 0.188792 = 0.173*(2.4^(2/3))/((0.007/0.019)^(2/3)).

How to calculate Pressure Coefficient for Blunt-Nosed Plate?

With Drag Coefficient (C_d), Distance from Y-Axis (x) & Diameter 1 (d₁) we can find Pressure Coefficient for Blunt-Nosed Plate using the formula - Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3)).

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=0.096*(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 for Blunt-Nosed Plate Formula

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

​GoPressure Coefficient for Blunt-Nosed Cylinder Formula

Pressure Coefficient for Blunt-Nosed Plate Example

Pressure Coefficient for Blunt-Nosed Plate Solution

Pressure Coefficient for Blunt-Nosed Plate Formula Elements

Other Formulas to find Pressure Coefficient

How to Evaluate Pressure Coefficient for Blunt-Nosed Plate?

FAQs on Pressure Coefficient for Blunt-Nosed Plate

Variable Name

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

GoPressure Coefficient for Blunt-Nosed Cylinder Formula