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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
Cp=2γM2(p-γM2λ2-1)
Cp - Pressure Coefficient?γ - Specific Heat Ratio?M - Mach Number?p- - Non Dimensionalized Pressure?λ - Slenderness Ratio?

Coefficient of Pressure with Slenderness Ratio Example

With values
With units
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Here is how the Coefficient of Pressure with Slenderness Ratio equation looks like with Values.

Here is how the Coefficient of Pressure with Slenderness Ratio equation looks like with Units.

Here is how the Coefficient of Pressure with Slenderness Ratio equation looks like.

2.0816Edit=21.1Edit5.4Edit2(0.81Edit1.1Edit5.4Edit20.2Edit2-1)
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Coefficient of Pressure with Slenderness Ratio Solution

Follow our step by step solution on how to calculate Coefficient of Pressure with Slenderness Ratio?

FIRST Step Consider the formula
Cp=2γM2(p-γM2λ2-1)
Next Step Substitute values of Variables
Cp=21.15.42(0.811.15.420.22-1)
Next Step Prepare to Evaluate
Cp=21.15.42(0.811.15.420.22-1)
Next Step Evaluate
Cp=2.0816210618182
LAST Step Rounding Answer
Cp=2.0816

Coefficient of Pressure with Slenderness Ratio 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: Cp
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Specific Heat Ratio
The Specific Heat Ratio of a gas is the ratio of the specific heat of the gas at a constant pressure to its specific heat at a constant volume.
Symbol: γ
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Mach Number
Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
Symbol: M
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Non Dimensionalized Pressure
Non Dimensionalized Pressure is the technique which can ease the analysis of the problem at hand and reduce the number of free parameters.
Symbol: p-
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Slenderness Ratio
The Slenderness Ratio is the ratio of the length of a column and the least radius of gyration of its cross section.
Symbol: λ
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.

Other Formulas to find Pressure Coefficient

​Go Coefficient of Pressure with Slenderness Ratio and Similarity Constant
Cp=2λ2γK2(γK2p--1)

Other formulas in Hypersonic Flow and Disturbances category

​Go Change in Velocity for Hypersonic Flow in X Direction
u'=vfluid-U
​Go Similarity Constant Equation with Slenderness Ratio
K=Mλ
​Go Density Ratio with Similarity Constant having Slenderness Ratio
ρratio=(γ+1γ-1)(11+2(γ-1)K2)
​Go Similarity Constant Equation using Wave Angle
Kβ=Mβ180π

How to Evaluate Coefficient of Pressure with Slenderness Ratio?

Coefficient of Pressure with Slenderness Ratio evaluator uses Pressure Coefficient = 2/Specific Heat Ratio*Mach Number^2*(Non Dimensionalized Pressure*Specific Heat Ratio*Mach Number^2*Slenderness Ratio^2-1) to evaluate the Pressure Coefficient, Coefficient of Pressure with Slenderness Ratio formula is defined as a dimensionless quantity that characterizes the pressure distribution around a body in hypersonic flow, taking into account the effects of slenderness ratio on the flow field and the resulting pressure forces. Pressure Coefficient is denoted by Cp symbol.

How to evaluate Coefficient of Pressure with Slenderness Ratio using this online evaluator? To use this online evaluator for Coefficient of Pressure with Slenderness Ratio, enter Specific Heat Ratio (γ), Mach Number (M), Non Dimensionalized Pressure (p-) & Slenderness Ratio (λ) and hit the calculate button.

FAQs on Coefficient of Pressure with Slenderness Ratio

What is the formula to find Coefficient of Pressure with Slenderness Ratio?
The formula of Coefficient of Pressure with Slenderness Ratio is expressed as Pressure Coefficient = 2/Specific Heat Ratio*Mach Number^2*(Non Dimensionalized Pressure*Specific Heat Ratio*Mach Number^2*Slenderness Ratio^2-1). Here is an example- 2.081621 = 2/1.1*5.4^2*(0.81*1.1*5.4^2*0.2^2-1).
How to calculate Coefficient of Pressure with Slenderness Ratio?
With Specific Heat Ratio (γ), Mach Number (M), Non Dimensionalized Pressure (p-) & Slenderness Ratio (λ) we can find Coefficient of Pressure with Slenderness Ratio using the formula - Pressure Coefficient = 2/Specific Heat Ratio*Mach Number^2*(Non Dimensionalized Pressure*Specific Heat Ratio*Mach Number^2*Slenderness Ratio^2-1).
What are the other ways to Calculate Pressure Coefficient?
Here are the different ways to Calculate Pressure Coefficient-
  • Pressure Coefficient=(2*Slenderness Ratio^2)/(Specific Heat Ratio*Hypersonic Similarity Parameter^2)*(Specific Heat Ratio*Hypersonic Similarity Parameter^2*Non Dimensionalized Pressure-1)OpenImg
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