Local Mach Number using Reynolds Number Equation at Transition Region Solution

STEP 0: Pre-Calculation Summary
Formula Used
Local Mach Number = Boundary-layer Momentum Reynolds number/100
Me = ReθT/100
This formula uses 2 Variables
Variables Used
Local Mach Number - Local Mach Number is the ratio of the free-stream flow to the local speed of sound.
Boundary-layer Momentum Reynolds number - Boundary-layer momentum Reynolds number is the reynolds number at the transition region near the boundary layer.
STEP 1: Convert Input(s) to Base Unit
Boundary-layer Momentum Reynolds number: 2000 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Me = ReθT/100 --> 2000/100
Evaluating ... ...
Me = 20
STEP 3: Convert Result to Output's Unit
20 --> No Conversion Required
FINAL ANSWER
20 <-- Local Mach Number
(Calculation completed in 00.005 seconds)

Credits

Creator Image
Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Verifier Image
Verified by Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has verified this Calculator and 300+ more calculators!

Hypersonic Transition Calculators

Static Velocity at Transition Point
​ Go Static Velocity = (Transition Reynolds Number*Static Viscosity)/(Static Density*Location Transition Point)
Static Density at Transition Point
​ Go Static Density = (Transition Reynolds Number*Static Viscosity)/(Static Velocity*Location Transition Point)
Location of Transition Point
​ Go Location Transition Point = (Transition Reynolds Number*Static Viscosity)/(Static Velocity*Static Density)
Transition Reynolds Number
​ LaTeX ​ Go Transition Reynolds Number = (Static Density*Static Velocity*Location Transition Point)/Static Viscosity

Local Mach Number using Reynolds Number Equation at Transition Region Formula

​Go
Local Mach Number = Boundary-layer Momentum Reynolds number/100
Me = ReθT/100

What is local mach?

The ratio of the free-stream flow to the local speed of sound. The speed of sound varies because of temperature changes around the aircraft, and thus the local Mach number may be more, less, or equal to the free-stream Mach number.

How to Calculate Local Mach Number using Reynolds Number Equation at Transition Region?

Local Mach Number using Reynolds Number Equation at Transition Region calculator uses Local Mach Number = Boundary-layer Momentum Reynolds number/100 to calculate the Local Mach Number, Local Mach Number using Reynolds Number Equation at Transition Region formula is defined as a dimensionless quantity that characterizes the compressibility of fluid flow in the transition region of a flat plate, providing a critical value for the onset of turbulence in viscous flow cases. Local Mach Number is denoted by Me symbol.

How to calculate Local Mach Number using Reynolds Number Equation at Transition Region using this online calculator? To use this online calculator for Local Mach Number using Reynolds Number Equation at Transition Region, enter Boundary-layer Momentum Reynolds number (ReθT) and hit the calculate button. Here is how the Local Mach Number using Reynolds Number Equation at Transition Region calculation can be explained with given input values -> 20 = 2000/100.

FAQ

What is Local Mach Number using Reynolds Number Equation at Transition Region?
Local Mach Number using Reynolds Number Equation at Transition Region formula is defined as a dimensionless quantity that characterizes the compressibility of fluid flow in the transition region of a flat plate, providing a critical value for the onset of turbulence in viscous flow cases and is represented as Me = ReθT/100 or Local Mach Number = Boundary-layer Momentum Reynolds number/100. Boundary-layer momentum Reynolds number is the reynolds number at the transition region near the boundary layer.
How to calculate Local Mach Number using Reynolds Number Equation at Transition Region?
Local Mach Number using Reynolds Number Equation at Transition Region formula is defined as a dimensionless quantity that characterizes the compressibility of fluid flow in the transition region of a flat plate, providing a critical value for the onset of turbulence in viscous flow cases is calculated using Local Mach Number = Boundary-layer Momentum Reynolds number/100. To calculate Local Mach Number using Reynolds Number Equation at Transition Region, you need Boundary-layer Momentum Reynolds number (ReθT). With our tool, you need to enter the respective value for Boundary-layer Momentum Reynolds number and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!