Pressure Coefficient for Blunt-Nosed Plate Calculator

✖The Drag Coefficient is a dimensionless quantity that characterizes the drag forces acting on an object in a blast wave, influencing its motion and trajectory.ⓘ Drag Coefficient [C_d]			+10% -10%
✖The Distance from Y-Axis is the perpendicular distance of a point from the Y-axis in the blast wave theory, used to analyze shockwave propagation.ⓘ Distance from Y-Axis [x]			+10% -10%
✖The Diameter 1 is the diameter of the first blast wave in the blast wave theory, which is a crucial parameter in explosion dynamics.ⓘ Diameter 1 [d₁]			+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 for Blunt-Nosed Plate [C_p]

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Pressure Coefficient for Blunt-Nosed Plate Solution

STEP 0: Pre-Calculation Summary

Formula Used

Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3))
C_p = 0.173*(C_d^(2/3))/((x/d₁)^(2/3))
This formula uses 4 Variables

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.
Drag Coefficient - The Drag Coefficient is a dimensionless quantity that characterizes the drag forces acting on an object in a blast wave, influencing its motion and trajectory.
Distance from Y-Axis - (Measured in Meter) - The Distance from Y-Axis is the perpendicular distance of a point from the Y-axis in the blast wave theory, used to analyze shockwave propagation.
Diameter 1 - (Measured in Meter) - The Diameter 1 is the diameter of the first blast wave in the blast wave theory, which is a crucial parameter in explosion dynamics.

STEP 1: Convert Input(s) to Base Unit

Drag Coefficient: 2.4 --> No Conversion Required
Distance from Y-Axis: 7 Millimeter --> 0.007 Meter (Check conversion here)
Diameter 1: 29.00368 Millimeter --> 0.02900368 Meter (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_p = 0.173*(C_d^(2/3))/((x/d₁)^(2/3)) --> 0.173*(2.4^(2/3))/((0.007/0.02900368)^(2/3))

Evaluating ... ...

C_p = 0.800000590416685

STEP 3: Convert Result to Output's Unit

0.800000590416685 --> No Conversion Required

FINAL ANSWER

0.800000590416685 ≈ 0.800001 <-- Pressure Coefficient

(Calculation completed in 00.020 seconds)

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Home » Engineering » Mechanical » Fluid Mechanics » Hypersonic Flow » Blast Wave Part Theory » Pressure Coefficient for Blunt-Nosed Plate

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

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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 for Blunt-Nosed Plate Formula

LaTeX Go

Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3))
C_p = 0.173*(C_d^(2/3))/((x/d₁)^(2/3))

What is Coefficient of Drag?

Coefficient of Drag is a dimensionless number that quantifies the drag or resistance of an object as it moves through a fluid, such as air or water, used in the drag equation to calculate the drag force acting on the object which depends on the shape, surface roughness, and flow conditions around the object.

What is Pressure Coefficient?

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

How to Calculate Pressure Coefficient for Blunt-Nosed Plate?

Pressure Coefficient for Blunt-Nosed Plate calculator uses Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3)) to calculate the Pressure Coefficient, Pressure Coefficient for Blunt-Nosed Plate formula is defined as a dimensionless quantity that characterizes the pressure distribution around a blunt-nosed plate in a blast wave, providing a crucial parameter in blast wave theory to estimate the pressure exerted on the plate. Pressure Coefficient is denoted by C_p symbol.

How to calculate Pressure Coefficient for Blunt-Nosed Plate using this online calculator? To use this online calculator 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. Here is how the Pressure Coefficient for Blunt-Nosed Plate calculation can be explained with given input values -> 0.603426 = 0.173*(2.4^(2/3))/((0.007/0.02900368)^(2/3)).

FAQ

What is Pressure Coefficient for Blunt-Nosed Plate?

Pressure Coefficient for Blunt-Nosed Plate formula is defined as a dimensionless quantity that characterizes the pressure distribution around a blunt-nosed plate in a blast wave, providing a crucial parameter in blast wave theory to estimate the pressure exerted on the plate and is represented as C_p = 0.173*(C_d^(2/3))/((x/d₁)^(2/3)) or Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3)). The Drag Coefficient is a dimensionless quantity that characterizes the drag forces acting on an object in a blast wave, influencing its motion and trajectory, The Distance from Y-Axis is the perpendicular distance of a point from the Y-axis in the blast wave theory, used to analyze shockwave propagation & The Diameter 1 is the diameter of the first blast wave in the blast wave theory, which is a crucial parameter in explosion dynamics.

How to calculate Pressure Coefficient for Blunt-Nosed Plate?

Pressure Coefficient for Blunt-Nosed Plate formula is defined as a dimensionless quantity that characterizes the pressure distribution around a blunt-nosed plate in a blast wave, providing a crucial parameter in blast wave theory to estimate the pressure exerted on the plate is calculated using Pressure Coefficient = 0.173*(Drag Coefficient^(2/3))/((Distance from Y-Axis/Diameter 1)^(2/3)). To calculate Pressure Coefficient for Blunt-Nosed Plate, you need Drag Coefficient (C_d), Distance from Y-Axis (x) & Diameter 1 (d₁). With our tool, you need to enter the respective value for Drag Coefficient, Distance from Y-Axis & Diameter 1 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 Drag Coefficient, Distance from Y-Axis & Diameter 1. We can use 3 other way(s) to calculate the same, which is/are as follows -

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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