Critical Density Solution

STEP 0: Pre-Calculation Summary
Formula Used
Critical Density = Stagnation Density*(2/(Specific Heat Ratio+1))^(1/(Specific Heat Ratio-1))
ρcr = ρo*(2/(γ+1))^(1/(γ-1))
This formula uses 3 Variables
Variables Used
Critical Density - (Measured in Kilogram per Cubic Meter) - Critical Density is defined as the density of the fluid at sonic conditions, when Mach number is one.
Stagnation Density - (Measured in Kilogram per Cubic Meter) - Stagnation Density is defined as the density of fluid at a stagnation point in a fluid flow.
Specific Heat Ratio - The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume of the flowing fluid for non-viscous and compressible flow.
STEP 1: Convert Input(s) to Base Unit
Stagnation Density: 1.22 Kilogram per Cubic Meter --> 1.22 Kilogram per Cubic Meter No Conversion Required
Specific Heat Ratio: 1.4 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
ρcr = ρo*(2/(γ+1))^(1/(γ-1)) --> 1.22*(2/(1.4+1))^(1/(1.4-1))
Evaluating ... ...
ρcr = 0.773404537217943
STEP 3: Convert Result to Output's Unit
0.773404537217943 Kilogram per Cubic Meter --> No Conversion Required
FINAL ANSWER
0.773404537217943 0.773405 Kilogram per Cubic Meter <-- Critical Density
(Calculation completed in 00.004 seconds)

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Created by Shikha Maurya
Indian Institute of Technology (IIT), Bombay
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Verified by Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
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Governing Equations and Sound Wave Calculators

Speed of Sound
​ Go Speed of Sound = sqrt(Specific Heat Ratio*[R-Dry-Air]*Static Temperature)
Mayer's Formula
​ LaTeX ​ Go Specific Gas Constant = Specific Heat Capacity at Constant Pressure-Specific Heat Capacity at Constant Volume
Mach Number
​ Go Mach Number = Speed of Object/Speed of Sound
Mach Angle
​ Go Mach Angle = asin(1/Mach Number)

Critical Density Formula

​LaTeX ​Go
Critical Density = Stagnation Density*(2/(Specific Heat Ratio+1))^(1/(Specific Heat Ratio-1))
ρcr = ρo*(2/(γ+1))^(1/(γ-1))

What is Critical Density?

In terminology of compressible flows, critical density refers to the mass per unit volume of the fluid at sonic conditions, i.e. when Mach number is 1.

How to Calculate Critical Density?

Critical Density calculator uses Critical Density = Stagnation Density*(2/(Specific Heat Ratio+1))^(1/(Specific Heat Ratio-1)) to calculate the Critical Density, The Critical Density at a point in a fluid flow is defined as the density that would exist if the flow became sonic at that point. Critical Density is denoted by ρcr symbol.

How to calculate Critical Density using this online calculator? To use this online calculator for Critical Density, enter Stagnation Density o) & Specific Heat Ratio (γ) and hit the calculate button. Here is how the Critical Density calculation can be explained with given input values -> 0.77416 = 1.22*(2/(1.4+1))^(1/(1.4-1)).

FAQ

What is Critical Density?
The Critical Density at a point in a fluid flow is defined as the density that would exist if the flow became sonic at that point and is represented as ρcr = ρo*(2/(γ+1))^(1/(γ-1)) or Critical Density = Stagnation Density*(2/(Specific Heat Ratio+1))^(1/(Specific Heat Ratio-1)). Stagnation Density is defined as the density of fluid at a stagnation point in a fluid flow & The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume of the flowing fluid for non-viscous and compressible flow.
How to calculate Critical Density?
The Critical Density at a point in a fluid flow is defined as the density that would exist if the flow became sonic at that point is calculated using Critical Density = Stagnation Density*(2/(Specific Heat Ratio+1))^(1/(Specific Heat Ratio-1)). To calculate Critical Density, you need Stagnation Density o) & Specific Heat Ratio (γ). With our tool, you need to enter the respective value for Stagnation Density & Specific Heat Ratio and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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