Coefficient of Pressure with Slenderness Ratio and Similarity Constant Calculator

✖The Slenderness Ratio is the ratio of the length of a column and the least radius of gyration of its cross section.ⓘ Slenderness Ratio [λ]			+10% -10%
✖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.ⓘ Specific Heat Ratio [γ]			+10% -10%
✖Hypersonic Similarity Parameter, In the study of hypersonic flow over slender bodies, the product M1u is an important governing parameter, where, as before. It is to simplify the equations.ⓘ Hypersonic Similarity Parameter [K]			+10% -10%
✖Non Dimensionalized Pressure is the technique which can ease the analysis of the problem at hand and reduce the number of free parameters.ⓘ Non Dimensionalized Pressure [p_-]			+10% -10%

✖Pressure coefficient defines the value of local pressure at a point in terms of free stream pressure and dynamic pressure.ⓘ Coefficient of Pressure with Slenderness Ratio and Similarity Constant [C_p]

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Coefficient of Pressure with Slenderness Ratio and Similarity Constant Solution

STEP 0: Pre-Calculation Summary

Formula Used

Pressure Coefficient = (2*Slenderness Ratio^2)/(Specific Heat Ratio*Hypersonic Similarity Parameter^2)*(Specific Heat Ratio*Hypersonic Similarity Parameter^2*Non Dimensionalized Pressure-1)
C_p = (2*λ^2)/(γ*K^2)*(γ*K^2*p_--1)
This formula uses 5 Variables

Variables Used

Pressure Coefficient - Pressure coefficient defines the value of local pressure at a point in terms of free stream pressure and dynamic pressure.
Slenderness Ratio - The Slenderness Ratio is the ratio of the length of a column and the least radius of gyration of its cross section.
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.
Hypersonic Similarity Parameter - (Measured in Radian) - Hypersonic Similarity Parameter, In the study of hypersonic flow over slender bodies, the product M1u is an important governing parameter, where, as before. It is to simplify the equations.
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.

STEP 1: Convert Input(s) to Base Unit

Slenderness Ratio: 0.2 --> No Conversion Required
Specific Heat Ratio: 1.1 --> No Conversion Required
Hypersonic Similarity Parameter: 1.396 Radian --> 1.396 Radian No Conversion Required
Non Dimensionalized Pressure: 0.81 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_p = (2*λ^2)/(γ*K^2)*(γ*K^2*p_--1) --> (2*0.2^2)/(1.1*1.396^2)*(1.1*1.396^2*0.81-1)

Evaluating ... ...

C_p = 0.0274813035569942

STEP 3: Convert Result to Output's Unit

0.0274813035569942 --> No Conversion Required

FINAL ANSWER

0.0274813035569942 ≈ 0.027481 <-- Pressure Coefficient

(Calculation completed in 00.004 seconds)

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Amrita School of Engineering (ASE), Vallikavu

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< Hypersonic Flow and Disturbances Calculators

Coefficient of Pressure with Slenderness Ratio

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

Density Ratio with Similarity Constant having Slenderness Ratio

LaTeX Go Density Ratio = ((Specific Heat Ratio+1)/(Specific Heat Ratio-1))*(1/(1+2/((Specific Heat Ratio-1)*Hypersonic Similarity Parameter^2)))

Change in Velocity for Hypersonic Flow in X Direction

LaTeX Go Change in Velocity for Hypersonic Flow = Fluid Velocity-Freestream Velocity Normal

Similarity Constant Equation with Slenderness Ratio

LaTeX Go Hypersonic Similarity Parameter = Mach Number*Slenderness Ratio

Coefficient of Pressure with Slenderness Ratio and Similarity Constant Formula

LaTeX Go

What is pressure coefficient?

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

How to Calculate Coefficient of Pressure with Slenderness Ratio and Similarity Constant?

Coefficient of Pressure with Slenderness Ratio and Similarity Constant calculator uses Pressure Coefficient = (2*Slenderness Ratio^2)/(Specific Heat Ratio*Hypersonic Similarity Parameter^2)*(Specific Heat Ratio*Hypersonic Similarity Parameter^2*Non Dimensionalized Pressure-1) to calculate the Pressure Coefficient, Coefficient of Pressure with Slenderness Ratio and Similarity Constant formula is defined as a dimensionless quantity that characterizes the pressure distribution around a body in hypersonic flow, taking into account the slenderness ratio and similarity constant, which are crucial in understanding disturbances in hypersonic flow. Pressure Coefficient is denoted by C_p symbol.

How to calculate Coefficient of Pressure with Slenderness Ratio and Similarity Constant using this online calculator? To use this online calculator for Coefficient of Pressure with Slenderness Ratio and Similarity Constant, enter Slenderness Ratio (λ), Specific Heat Ratio (γ), Hypersonic Similarity Parameter (K) & Non Dimensionalized Pressure (p_-) and hit the calculate button. Here is how the Coefficient of Pressure with Slenderness Ratio and Similarity Constant calculation can be explained with given input values -> 0.027481 = (2*0.2^2)/(1.1*1.396^2)*(1.1*1.396^2*0.81-1).

FAQ

What is Coefficient of Pressure with Slenderness Ratio and Similarity Constant?

Coefficient of Pressure with Slenderness Ratio and Similarity Constant formula is defined as a dimensionless quantity that characterizes the pressure distribution around a body in hypersonic flow, taking into account the slenderness ratio and similarity constant, which are crucial in understanding disturbances in hypersonic flow and is represented as C_p = (2*λ^2)/(γ*K^2)*(γ*K^2*p_--1) or Pressure Coefficient = (2*Slenderness Ratio^2)/(Specific Heat Ratio*Hypersonic Similarity Parameter^2)*(Specific Heat Ratio*Hypersonic Similarity Parameter^2*Non Dimensionalized Pressure-1). The Slenderness Ratio is the ratio of the length of a column and the least radius of gyration of its cross section, 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, Hypersonic Similarity Parameter, In the study of hypersonic flow over slender bodies, the product M1u is an important governing parameter, where, as before. It is to simplify the equations & Non Dimensionalized Pressure is the technique which can ease the analysis of the problem at hand and reduce the number of free parameters.

How to calculate Coefficient of Pressure with Slenderness Ratio and Similarity Constant?

Coefficient of Pressure with Slenderness Ratio and Similarity Constant formula is defined as a dimensionless quantity that characterizes the pressure distribution around a body in hypersonic flow, taking into account the slenderness ratio and similarity constant, which are crucial in understanding disturbances in hypersonic flow is calculated using Pressure Coefficient = (2*Slenderness Ratio^2)/(Specific Heat Ratio*Hypersonic Similarity Parameter^2)*(Specific Heat Ratio*Hypersonic Similarity Parameter^2*Non Dimensionalized Pressure-1). To calculate Coefficient of Pressure with Slenderness Ratio and Similarity Constant, you need Slenderness Ratio (λ), Specific Heat Ratio (γ), Hypersonic Similarity Parameter (K) & Non Dimensionalized Pressure (p_-). With our tool, you need to enter the respective value for Slenderness Ratio, Specific Heat Ratio, Hypersonic Similarity Parameter & Non Dimensionalized Pressure 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 Slenderness Ratio, Specific Heat Ratio, Hypersonic Similarity Parameter & Non Dimensionalized Pressure. We can use 1 other way(s) to calculate the same, which is/are as follows -

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

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