1. Boundary layer concept

2. Laminar flow

3. Laminar Boundary Layer Flow
The laminar boundary layer is a very smooth flow, while the turbulent boundary layer contains swirls or “eddies.”
The laminar flow creates less skin friction drag than the turbulent flow, but is less stable.
Boundary layer flow over a wing surface begins as a smooth laminar flow. As the flow continues back from the leading edge, the laminar boundary layer increases in thickness.

4. Turbulent Boundary Layer Flow
At some distance back from the leading edge, the smooth laminar flow breaks down and transitions to a turbulent flow.
From a drag standpoint, it is advisable to have the transition from laminar to turbulent flow as far aft on the wing as possible, or have a large amount of the wing surface within the laminar portion of the boundary layer.
The low energy laminar flow, however, tends to break down more suddenly than the turbulent layer.

8. Flow through the pipes in series

9. Pipes in series is defined as the pipes of different lengths and different diameters connected end to end to form a pipe line.
L1,L2,L3 = length of pipes 1,2 and 3
d1,d2,d3 = diameter of pipes 1,2,3
v1,v2,v3 = velocity of flow through pipes 1,2,3
f1,f2,f = coefficient of frictions for pipes 1,2,3
H = difference of water level in the two tanks
The discharge passing through the pipe is same.
Q=A1V1=A2V2=A3V3
The difference in liquid surface levels is equal to the sum of the total head loss in the pipes

11. Parallel pipe system
Consider a main pipe which divide into two or more branches as shown in figure
Again join together downstream to form a single pipe then the branch pipes are said to be connected in parallel. The discharge through the main is increased by connecting pipes in parallel
the rate of flow in the main pipe is equal to the sum of rate of flow through branch pipes.
hence
Q =Q1+ Q2

12. In this arrangement loss of head for each pipe is same
Loss of head for branch pipe1=loss of head for branch pipe 2

13. Moody Diagram that can be used to estimate friction coefficients
The Moody friction factor - λ (or f) - is used in the Darcy-Weisbach major loss equation
If the flow is transient < Re < the flow varies between laminar and turbulent flow and the friction coefficient is not possible to determine.
The friction factor can usually be interpolated between the laminar value at Re = 2300 and the turbulent value at Re = 4000

14. Moody diagram

15. Total energy gradient line

16. Total energy gradient line is equal to sum of pressure head ,velocity head and datum head
EL = H = p / W + v2 / 2 g + h = constant along a streamline        
where
(EL ) Energy Line
For a fluid flow without any losses due to friction (major losses) or components (minor losses) - the energy line would be at a constant level. In a practical world the energy line decreases along the flow due to losses.
A turbine in the flow reduces the energy line and a pump or fan in the line increases the energy line

17. Hydraulic gradient line is the sum of pressure head and datum head
Hydraulic Grade Line (HGL )
Hydraulic gradient line is the sum of pressure head and datum head
HGL = p / W + h        
where
The hydraulic grade line lies one velocity head below the energy line.