Characteristic Mach Number Solution

STEP 0: Pre-Calculation Summary
Formula Used
Characteristic Mach Number = Fluid Velocity/Critical Speed of Sound
Mcr = uf/acr
This formula uses 3 Variables
Variables Used
Characteristic Mach Number - Characteristic Mach number is defined as the speed of an object to the speed of sound at the sonic condition.
Fluid Velocity - (Measured in Meter per Second) - Fluid Velocity is the volume of fluid flowing in the given vessel per unit cross sectional area.
Critical Speed of Sound - (Measured in Meter per Second) - The Critical Speed of Sound is defined as the speed of sound at critical conditions in fluid flow.
STEP 1: Convert Input(s) to Base Unit
Fluid Velocity: 12 Meter per Second --> 12 Meter per Second No Conversion Required
Critical Speed of Sound: 79.741 Meter per Second --> 79.741 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Mcr = uf/acr --> 12/79.741
Evaluating ... ...
Mcr = 0.150487202317503
STEP 3: Convert Result to Output's Unit
0.150487202317503 --> No Conversion Required
FINAL ANSWER
0.150487202317503 0.150487 <-- Characteristic Mach Number
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
Verifier Image
Verified by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has verified this Calculator and 200+ more calculators!

Normal Shock Relations Calculators

Relation between Mach Number and Characteristic Mach Number
​ LaTeX ​ Go Characteristic Mach Number = ((Specific Heat Ratio+1)/(Specific Heat Ratio-1+2/(Mach Number^2)))^0.5
Downstream Velocity using Prandtl Relation
​ LaTeX ​ Go Velocity Downstream of Shock = (Critical Speed of Sound^2)/Velocity Upstream of Shock
Upstream Velocity using Prandtl Relation
​ LaTeX ​ Go Velocity Upstream of Shock = (Critical Speed of Sound^2)/Velocity Downstream of Shock
Characteristic Mach Number
​ LaTeX ​ Go Characteristic Mach Number = Fluid Velocity/Critical Speed of Sound

Characteristic Mach Number Formula

​LaTeX ​Go
Characteristic Mach Number = Fluid Velocity/Critical Speed of Sound
Mcr = uf/acr

What is the difference between Mach number and Characteristic Mach number?

Characteristic Mach number varies qualitative same as the actual Mach number except that the characteristic Mach number reaches to finite value when actual Mach number reaches infinity.

How to Calculate Characteristic Mach Number?

Characteristic Mach Number calculator uses Characteristic Mach Number = Fluid Velocity/Critical Speed of Sound to calculate the Characteristic Mach Number, Characteristic Mach Number formula is defined as the ratio of flow velocity to the speed of sound in a compressible flow, providing insight into the behavior of shock waves and the flow characteristics in aerospace applications. Characteristic Mach Number is denoted by Mcr symbol.

How to calculate Characteristic Mach Number using this online calculator? To use this online calculator for Characteristic Mach Number, enter Fluid Velocity (uf) & Critical Speed of Sound (acr) and hit the calculate button. Here is how the Characteristic Mach Number calculation can be explained with given input values -> 0.150487 = 12/79.741.

FAQ

What is Characteristic Mach Number?
Characteristic Mach Number formula is defined as the ratio of flow velocity to the speed of sound in a compressible flow, providing insight into the behavior of shock waves and the flow characteristics in aerospace applications and is represented as Mcr = uf/acr or Characteristic Mach Number = Fluid Velocity/Critical Speed of Sound. Fluid Velocity is the volume of fluid flowing in the given vessel per unit cross sectional area & The Critical Speed of Sound is defined as the speed of sound at critical conditions in fluid flow.
How to calculate Characteristic Mach Number?
Characteristic Mach Number formula is defined as the ratio of flow velocity to the speed of sound in a compressible flow, providing insight into the behavior of shock waves and the flow characteristics in aerospace applications is calculated using Characteristic Mach Number = Fluid Velocity/Critical Speed of Sound. To calculate Characteristic Mach Number, you need Fluid Velocity (uf) & Critical Speed of Sound (acr). With our tool, you need to enter the respective value for Fluid Velocity & Critical Speed of Sound 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 Characteristic Mach Number?
In this formula, Characteristic Mach Number uses Fluid Velocity & Critical Speed of Sound. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Characteristic Mach Number = ((Specific Heat Ratio+1)/(Specific Heat Ratio-1+2/(Mach Number^2)))^0.5
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!