# Boundary Layer Study Notes for Mechanical Engineering

By Vijay Pratap Singh|Updated : December 3rd, 2021

Introduction

The boundary layer phenomenon occurs when a fluid flows over a flat plate causing laminar or turbulent flow. This topic defines various parameters such as Energy thickness, Momentum thickness, Boundary layer thickness etc.

Introduction

Boundary layer phenomenon occurs when a fluid flows over a flat plate causing laminar or turbulent flow. This topic defines various parameters such as Energy thickness, Momentum thickness, Boundary layer thickness etc.

Boundary layer theory

• Boundary layer theory was developed by Prandtl in the year 1904.
• When a real fluid flows over a solid body, the velocity of the fluid at the boundary will be zero. If the boundary is stationary.
• As we move away from the boundary in the perpendicular direction, velocity increases to the free stream velocity. It means velocity gradient  will exist.

Note: velocity gradient  does not exist outside the boundary layer as outside the boundary layer velocity is constant and equal to free stream velocity.

Boundary Layer Thickness (δ): It is the distance from the boundary to the point where velocity of fluid is approximately equal to 99% of free stream velocity. It is represented by δ.

Development of Boundary Layer: Development of boundary layer can be divided in three regions: laminar, transition, turbulent.

Boundary conditions:

(i) at y = 0, u = 0

(ii) y = δ, u = u

(iii) y = δ, =0

(iv) x = 0, δ = 0

Here, x is distance from leading edge in horizontal direction.

Reynolds number (Re

For laminar boundary layer (Re)x < 5 × 105 (For flat plate)

For turbulent boundary layer (Re)x > 5 × 105 (For flat plate)

Displacement Thickness (δ*): It is observed that inside the boundary layer velocity of fluid is less than free stream velocity hence, discharge is less in this region. To compensate for reduction in discharge the boundary is displaced outward in perpendicular direction by some distance. This distance is called displacement thickness (δ*).

Momentum Thickness (δ**  or θ): As due to boundary layer reduction in velocity occurs, so momentum also decreases. Momentum thickness is defined as the distance measured normal to boundary of solid body by which the boundary should be displaced to compensate for the reduction in momentum of flowing fluid.

Energy Thickness (δe): It is defined as distance measured perpendicular to the boundary of solid body by which the boundary should be displaced to compensate for reduction in kinetic energy of flowing fluid (KE decreases due to formation of boundary layer)

Shape Factor(H):

• It is defined as the ratio of displacement thickness to momentum thickness.
• Hence: H=δ*/θ
• This ratio depends solely on the shape of the velocity profile.

Laminar Flow: A flow in which fluid flows in layer and no intermixing with each other is known as laminar flow.

For circular pipe, flow will be laminar,

Where, ρ = Density of fluid, v = Velocity of fluid, D = Diameter of pipe, μ = Viscosity of fluid.

For flat plate flow will be laminar,

Where, L is length of plate.

Turbulent Flow: In this flow, adjacent layer of fluid cross each other (particles of fluid move randomly instead of moving in stream line path).

For flow inside pipe flow will be turbulent, If Re > 4000

for flat plate flow will be turbulent, If Re > 5 × 105

Von Karman Momentum Integral Equation

where, θ = momentum thickness; ρ = Density of fluid.

This is applied to:
1. Laminar boundary layers,
2. Transition boundary layers, and
3. Turbulent boundary layer flows.

Shear stress:

where, U = Free stream velocity

Local Coefficient of Drag (C*D): It is defined as the ratio of the shear stress τ0 to the quantity

It is denoted by

Average Coefficient of Drag (CD): It is defined as the ratio of the total drag force to

It is denoted by

Where, A = Area of surface, U = Free stream velocity, ρ = Mass density of fluid.

Total drag on a flat plate due to laminar and turbulent boundary layer:-

Total drag= Laminar drag upto tansition boundary + turbulent drag for whole plate - turbulent drag upto transition boundary

Drag force=FD = ½ ρ * v2 * CD * A

Blassius Experiment Results

where x = Distance from leading edge

Rex = Reynold number for length x.

ReL = Reynold number at end of plane

For laminar flow, Boundary layer thickness  δ ∝ √x

Shear stress at solid surface

Velocity profile for turbulent boundary layer on Flate surface is

where n =1/7  for Re < 107 but more than 5 × 105

Boundary Layer Separation:

Let us take curve surface ABCSD where fluid flow separation point S is determined from the condition

If  the flow is separated

If  the flow is on the average of separation

If  the flow will not separate or flow will remain attained

Methods of Preventing Separation of Boundary Layer:

Suction of slow moving fluid by a suction slot.

• Supplying additional energy from a blower.
• Providing a bypass in the slotted
• Rotating boundary in the direction of flow.
• Providing small divergence in diffuser.
• Providing guide blades in a bend.
• Providing a trip wire ring in the laminar region for the flow over a sphere.

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### Comments

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Sudhakar MalothJul 12, 2018

Sir send me IES material

Abinash KumarJul 12, 2018

Guys if you wants to clear gate exam follow the books....only..gade up is best suiyable for quizes......thanku...and best of luck.....

Rohit DhimanJul 13, 2018

This is just catalyst, I will enhance ur prep

Rohit DhimanJul 13, 2018

It*

Akshay MauryaJul 14, 2018

Sir why in boundary condition dy/dy is zero when u and y =0

Arnav SinghAug 8, 2019

made easy handbook hai ye to..... aur favourable pressure gradient galat hai at the verge of flow

Mahesh NanavareAug 11, 2019

dp/dx >0 (+ve slope) this should be the expression for D section in diagram of separation of boundary layer.

Chirag ShahAug 16, 2019

This comment is hidden because it was marked spam.

Vijay ChollangiJul 29, 2020

Thank you sir🙂👍👍

Daya VasuDec 26, 2021

Good ..

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