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HYDRAULIC 1 CVE 303 Powered By Docstoc
   CVE 303
   Types of flow – The type of flow depends on the manner in which the particles
    unite, the particles group themselves in a variety of ways e.g. regular or irregular.
    The type of flow is identified by the Reynolds number.

                      R 
    Flow of an IDEAL FLUID – No Viscousity
    Flow of a REAL FLUID – Viscousity included
   Laminar (low velocity, motion in layers) &
   Turbulent Flow ( high velocity, chaotic motion)
   Steady flow (conditions at any point remain constant, may differ from point to point)
   Uniform Flow ( velocity is the same at any given point in the fluid)
   Flow lines : Path lines, Stream lines and Streak lines
   Straight line streamlines of moving particle- One dimensional flow (Flow in pipes)
   Curve – Two dimensional flow (Flow over a spillway)
   Streamlines represented in space – Three dimensional (flow in a river bed)
   Motion of Fluid Particles
        Lagrangian method
        Eulerian method
Equation of continuity of a liquid flow: If an incompressible liquid us
    is continuously flowing through a pipe or a channel (whose cross-sectional area
    may or may not be constant) the quantity of liquid passing per second is the
    same at all sections.
                     Q1  Q2  Q3
                     a1v1  a2 v2  a3v3

 Water is flowing through a tapered pipe having end
  diameter of 150m and 50m respectively. Find the discharge
  at the larger end and velocity head at the smaller end if the
  velocity of water at the larger end is 2m/s.

   A circular pipe of 250 mm diameter carries an oil of specific
    gravity 0.8 at the rate of 120 litres/s and under a pressure
    of 20kPa. Calculate the total energy in meters at a point
    which is 3m above the datum line.

   A horizontal pipe 100 m long uniformly tapers from 300
    mm diameter to 200 mm diameter. What is the pressure
    head at the smaller end, if the pressure at the larger end is
    100 KPa and the pipe is discharging 50 litres of water per
    second. (5 marks

 Introduction
Energy of liquid in motion
      Potential: Energy a liquid posses by virtue of its position
      Kinetic: Energy posessed by a liquid by virtue of its motion
      Pressure head of a liquid particle in motion

   Total Energy : This is the sum of      a liquids Potential, Kinetics and
    Pressure energy

                         v2   p
                 E  Z     
                         2g   w
   Total Head of a liquid in motion
                                  v    p
                      H  Z         
                                  2g   w
   Definition: For a perfect incompressible fluid, flowing in
    a continuous stream, the total energy of a particle remains
    the same, while the particles moves from one point to
   Limitations of Bernoulli’s equation

   Practical application of Bernoulli’s equation
       Venturimeter ( Convergent cone, throat, divergent cone)
           Discharge through a venturimeter
                   Q  c.a2 .v2              2 gh
                                    a1  a2
                                     2    2

           Inclined venturimeter
     Orificemeter
     Pitot tube
   A pipe 500 m long has a slope of 1 in 100 and tapers from 1 m
    diameter at the higher end to 0.5 m at the lower end. The
    quantity of water flowing is 900 l/sec. If the pressure at the higher
    end is 70KPa. Find the pressure at the lower end.

   A pipe AB branches into two pipes C and D. The pipe has a
    diameter of 0.45 m at A, 0.3 m at B, 0.2 m at C and 0.15 m at D.
    Find the discharge at A if the velocity of water at A is 2 m/s also
    find the velocities at B and D if the velocity at C is 4 m/s.

   A venturimeter with a 150 mm diameter at inlet and 100 mm at
    throat is laid with its axis horizontal and is used for measuring
    the flow of oil specific gravity 0.9. The oil mercury differential
    manometer shows a guage difference of 200 mm. Assume
    coefficient of meter as 0.98. Calculate the discharge in litres per
   A venturimeter has 400 mm diameter at the main and 150
    mm at the throat. If the difference of pressure is 250 mm of
    mercury and the metre coefficient is 0.97, calculate the
    discharge of oil (specific gravity = 0.75) through the
   General Definition: An         open channel is a passage through which the water flows under the
    force of gravity and atmospheric pressure e.g. canals, sewers, aqauduct. It is also known as free-
    surface flow or gravity flow. The flow here is not due to pressure as in the case of pipe flow. Most
    open channel flow are turbulent flow and froude number is the relevant parameter here
   Types of open channel flow
   Natural streams and rivers
   Artificial canals, flumes
   Sewers, tunnels, partially full pipelines
   Gutters
Applications of artificial channels
   Water power development
   Irrigation
   Water supply
   Drainage
   Flood control
   Reynolds no. for pipes                 IR pipe 

   Reynolds no. for open channels          IRchannel 
                                                                  ; Rn 
                                                                          P

   Wetted perimeter: Length of cross-sectional border in contact with water.              Length where
    friction acts.

   Slopes in open channel flow
   Uniform flow through open channels
        Chezy’s formula
                 V  C Rn So

      Values of Chezy’s constant in the formula for
       discharge in open channel
      Mannings formula
                       1 2 3 12
                  V     Rn S o

      Basin’s formula
      Kutter’s formula

   Geometric properties of cross-sections
   Trapezoidal channels
   Triangular channels
   Rectangular channels
 A trapezoidal channel 3.5 m wide at the bottom
  has side and bed slopes of 1:1 and 1:1000
  respectively. Using manning’s formula, find the
  discharge through the channel, if the depth of
  water is 0.5 m. Take N = 0.03.
 A non symmetrical trapezoidal cross-section with
  b = 1.2 m, m1 = 2 and m2 = 1, So = 0.00009, Q =
  120 m3/s and y = 0.6 m, find the manning’s
  roughness factor n.
 Unnatural stream’s cross-section can be
  approximated by a parabolic shape with B = 4m
  and a depth y = 2 m. If the stream is laid on a
  slope of 0.001 m/m and n = 0.028, determine the
   Introduction
                 v2       q3
          E  y     y
                 2g      2 gy 2
   Specific energy diagram
   Critical conditions
   E = Emin i.e.        dE
    Critical depth             q2
                        yc  3
   Critical velocity               q
                            vc         gyc
        Subcritical: y1 > yc tranquil, upper stage flow V < Vc
        Supercritical: y1 < yc rapid, lower stage flow V >Vc
   Froude’s number
   Critical depth in non rectangular channels
   Occurrence of critical flow
   Critical energy

          yc      Ec  2 Emin
                 3       3
           qmax  gyc

   Occurrence of Critical Flow
   Change from mild to steep slope in a channel
   Entrance from a reservoir into a steep slope channel
   Free fall from mild slope channel
   Free fall from steep slope channel

   Humps and Contractions

   A rectangular channel 3.25 m wide discharges 2600 litres of water per second.
    What is the critical depth and critical velocity?
   A channel of rectangular section 8 m wide is discharging water at the
    rate of 12 m3/s with an average velocity of 1.2 m/s. Find the type of
   A rectangular channel 3 m wide carries 4 m3/s of water in subcritical
    uniform flow at a depth of 1.2 m, a frictionless hump is to be installed
    across the bed. Find the critical hump height?
   Introduction : Local non-uniform flow phenomenon –
    supercritical flow going into subcritical. The shooting flow is an
    unstable type of flow and does not continue on the downstream
    side, the flow transform itself to the streaming flow by increasing
    its depth. The rise in water level which occurs during the
    transformation of the unstable shooting flow to the stable
    streaming flow is called hydraulic jump.
 Depth relations
 Energy losses                     hij   
                                             y2  y1 3
                                                4 y1 y2
                          v2          v2 
          H1  H 2   d1  1    d 2  2 
                          2g  
                                       2g 

 Types of jumps
 Stilling basins
   A horizontal rectangular channel of constant breadth has a
    sluice opening from the bed upwards. When the sluice is
    partially opened water issues at 6 m/s with a depth of 600
    mm. Determine the loss of head per KN of water.

    A discharge of 1000 l/s flows along a rectangular channel
    1.5 m wide. If a standing wave is to be formed at a point
    where the upstream depth is 180 mm. What would be the
    rise in water level?

   Water flows at the rate of 1 m3/s along a channel of
    rectangular section of 1.6 m width. If a standing wave
    occurs at a point where upstream depth is 250 mm. Find
    the rise in water level after the hydraulic jump. Also find
    the loss of head in the standing wave.

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