Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point Calculator

✖The Reynolds Number is a dimensionless quantity that helps predict flow patterns in different fluid flow situations, particularly in hypersonic transitions over flat plates.ⓘ Reynolds Number [Re]			+10% -10%
✖The Static Viscosity is a measure of a fluid's resistance to flow and deformation under shear stress, particularly relevant in hypersonic transition scenarios.ⓘ Static Viscosity [μe]			+10% -10%
✖The Static Velocity is the velocity of a fluid at a specific point in a flow field, measured relative to the surrounding fluid at rest.ⓘ Static Velocity [u_e]			+10% -10%
✖The Static Density is the mass per unit volume of a fluid at rest, crucial for understanding fluid behavior in hypersonic flow conditions.ⓘ Static Density [ρ_e]			+10% -10%

✖The Boundary-Layer Momentum Thickness for Transition is a measure of the thickness of the boundary layer where viscous effects influence flow behavior during hypersonic transition.ⓘ Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point [θt]

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Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point Solution

STEP 0: Pre-Calculation Summary

Formula Used

Boundary-Layer Momentum Thickness for Transition = (Reynolds Number*Static Viscosity)/(Static Velocity*Static Density)
θt = (Re*μe)/(u_e*ρ_e)
This formula uses 5 Variables

Variables Used

Boundary-Layer Momentum Thickness for Transition - (Measured in Meter) - The Boundary-Layer Momentum Thickness for Transition is a measure of the thickness of the boundary layer where viscous effects influence flow behavior during hypersonic transition.
Reynolds Number - The Reynolds Number is a dimensionless quantity that helps predict flow patterns in different fluid flow situations, particularly in hypersonic transitions over flat plates.
Static Viscosity - (Measured in Pascal Second) - The Static Viscosity is a measure of a fluid's resistance to flow and deformation under shear stress, particularly relevant in hypersonic transition scenarios.
Static Velocity - (Measured in Meter per Second) - The Static Velocity is the velocity of a fluid at a specific point in a flow field, measured relative to the surrounding fluid at rest.
Static Density - (Measured in Kilogram per Cubic Meter) - The Static Density is the mass per unit volume of a fluid at rest, crucial for understanding fluid behavior in hypersonic flow conditions.

STEP 1: Convert Input(s) to Base Unit

Reynolds Number: 6000 --> No Conversion Required
Static Viscosity: 11.2 Poise --> 1.12 Pascal Second (Check conversion here)
Static Velocity: 8.8 Meter per Second --> 8.8 Meter per Second No Conversion Required
Static Density: 98.3 Kilogram per Cubic Meter --> 98.3 Kilogram per Cubic Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

θt = (Re*μe)/(u_e*ρ_e) --> (6000*1.12)/(8.8*98.3)

Evaluating ... ...

θt = 7.76842689355406

STEP 3: Convert Result to Output's Unit

7.76842689355406 Meter --> No Conversion Required

FINAL ANSWER

7.76842689355406 ≈ 7.768427 Meter <-- Boundary-Layer Momentum Thickness for Transition

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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< Hypersonic Transition Calculators

Static Velocity at Transition Point

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

Static Density at Transition Point

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

Location of Transition Point

LaTeX 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

Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point Formula

LaTeX Go

Boundary-Layer Momentum Thickness for Transition = (Reynolds Number*Static Viscosity)/(Static Velocity*Static Density)
θt = (Re*μe)/(u_e*ρ_e)

What is Transition Reynolds Number?

Transitional or transient flow is the phase of flow that occurs between laminar and turbulent flow and corresponds to Reynolds numbers that land between 2300 and 4000. In this type of flow, there is a mixture of laminar and turbulent flows present.

How to Calculate Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point?

Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point calculator uses Boundary-Layer Momentum Thickness for Transition = (Reynolds Number*Static Viscosity)/(Static Velocity*Static Density) to calculate the Boundary-Layer Momentum Thickness for Transition, Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point formula is defined as a measure of the momentum thickness of a boundary layer at the transition point from laminar to turbulent flow, which is a critical parameter in understanding the behavior of fluid flow over a flat plate in viscous flow cases. Boundary-Layer Momentum Thickness for Transition is denoted by θt symbol.

How to calculate Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point using this online calculator? To use this online calculator for Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point, enter Reynolds Number (Re), Static Viscosity (μe), Static Velocity (u_e) & Static Density (ρ_e) and hit the calculate button. Here is how the Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point calculation can be explained with given input values -> 7.768427 = (6000*1.12)/(8.8*98.3).

FAQ

What is Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point?

Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point formula is defined as a measure of the momentum thickness of a boundary layer at the transition point from laminar to turbulent flow, which is a critical parameter in understanding the behavior of fluid flow over a flat plate in viscous flow cases and is represented as θt = (Re*μe)/(u_e*ρ_e) or Boundary-Layer Momentum Thickness for Transition = (Reynolds Number*Static Viscosity)/(Static Velocity*Static Density). The Reynolds Number is a dimensionless quantity that helps predict flow patterns in different fluid flow situations, particularly in hypersonic transitions over flat plates, The Static Viscosity is a measure of a fluid's resistance to flow and deformation under shear stress, particularly relevant in hypersonic transition scenarios, The Static Velocity is the velocity of a fluid at a specific point in a flow field, measured relative to the surrounding fluid at rest & The Static Density is the mass per unit volume of a fluid at rest, crucial for understanding fluid behavior in hypersonic flow conditions.

How to calculate Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point?

Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point formula is defined as a measure of the momentum thickness of a boundary layer at the transition point from laminar to turbulent flow, which is a critical parameter in understanding the behavior of fluid flow over a flat plate in viscous flow cases is calculated using Boundary-Layer Momentum Thickness for Transition = (Reynolds Number*Static Viscosity)/(Static Velocity*Static Density). To calculate Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point, you need Reynolds Number (Re), Static Viscosity (μe), Static Velocity (u_e) & Static Density (ρ_e). With our tool, you need to enter the respective value for Reynolds Number, Static Viscosity, Static Velocity & Static Density 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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