Chapter 4: Non uniform flow in open channels - PowerPoint PPT Presentation

1 / 57
About This Presentation
Title:

Chapter 4: Non uniform flow in open channels

Description:

Chapter 4: Non uniform flow in open channels Free Outfall from a Channel with a Mild Slope If slope s of the channel is less than sc the upstream flow will be tranquil. – PowerPoint PPT presentation

Number of Views:140
Avg rating:3.0/5.0
Slides: 58
Provided by: UiTM1
Category:

less

Transcript and Presenter's Notes

Title: Chapter 4: Non uniform flow in open channels


1
Chapter 4Non uniform flow in open channels
2
Learning outcomes
  • By the end of this lesson, students should be
    able to
  • Relate the concept of specific energy and
    momentum equations in the effect of change in bed
    level - Broad Crested Weir
  • Relate the concept of specific energy and
    momentum equations in the effect of lateral
    contraction of channel ( Venturi Flume)

3
Introduction
  • Analysis of steady non uniform flow in open
    channels.
  • Non uniform flow occurs in transitions where
    there is change in cross section or obstruction
    in channel.
  • Analysis requires a different approach, requiring
    the use of the energy equation in a different
    form.

4
Specific energy alternative depths of flow
  • Specific energy, E,
  • (16.1)
  • For a wide rectangular channel, mean velocity is,
  • While the volume rate of flow per unit width,

5
  • Substituting v q into E,
  • (16.2)
  • (16.3)
  • This equation has 3 roots
  • 1 root is negative unreal
  • 2 roots are positive real, which give 2
    alternate depths
  • Larger depth deep slow flow (subcritical/
    tranquil/ streaming flow).
  • Smaller depth shallow fast flow (supercritical/
    shooting flow)

6
(No Transcript)
7
(No Transcript)
8
  • Critical depth, DC
  • Depth at which the 2 roots coincide
  • q qmax
  • E Emin
  • To find DC
  • When dE/dD 0,
  • (16.4)

9
  • Sub. from (16.4) to (16.2),
  • Therefore, for rectangular channel,
  • Differentiating (16.3) assuming E is constant
  • (16.5)

10
  • When , (16.5) becomes,
  • Or (16.6)

11
  • Critical velocity velocity of flow corresponding
    to critical depth.
  • Sub. into (16.1),

12
DC for non rectangular sections
13
  • For any shape and cross sectional area the E for
    any D,
  • Since v Q/A,
  • (16.7)

14
  • For flow at DC and vC, Emin, differentiating
    (16.7),
  • (16.8)
  • But a change in depth will produce a change in
    cross-sectional area, therefore dA/dDB.
  • (16.9)

15
  • For critical flow,
  • From (16.9)
  • (16.10)
  • where is the average depth.

16
Froude Number
  • Assume a surface wave of height dZ is propagated
    from left to right of observer.
  • Wave is brought to rest relative to observer by
    imposing a velocity c equal to wave velocity on
    the observer, flow will appear steady.

17
(No Transcript)
18
  • Sub. du to (5.32),
  • If wave height dZ is small,

19
  • Ratio of the stream velocity u to the propagation
    velocity c-u is known as Froude Number Fr.
  • (5.34)
  • Fr can be used to determine the type of flow for
    open channel.

20
  • For critical flow conditions, the Froude Number
    is,
  • If v lt vc subcritical flow
  • If v gt vc supercritical flow
  • Important difference,
  • Subcritical disturbances can travel upstream
    and downstream thus enabling downstream
    conditions to determine the behavior of the flow.
  • Supercritical disturbances cannot travel
    upstream and thus downstream cannot control the
    behavior of the flow.

21
Tranquil Critical Shooting
Subcritical Critical Supercritical
Depth D gt DC D DC D lt DC
Velocity v lt vC v vC v gt vC
Fr Fr lt 1 Fr 1 Fr gt 1
Channel slope Mild Critical Steep
Control Downstream - Upstream
Disturbance Wave can travel upstream Standing waves Waves cannot travel upstream
22
  • Figure 4.1 shows that when flow is in the region
    of
  • Dc , small changes of E and q results in
    relatively large changes in D.
  • Small surface waves are therefore easily formed
    but since velocity of propagation vp vc, these
    waves will be stationary or standing waves.
  • Their presence therefore, an indication of
    critical flow conditions

23
  • Figure 4.1a Plot of D vs q for a constant E

24
  • Line OA from figure below can be drawn at 45
    through the origin.
  • If scales for E and D are the same, horizontal
    distances from vertical axis to line OA will be
    equal to D, and the distance from OA to the
    specific energy curve will be v2/2g.
  • If q is constant,
  • Tranquil flow
  • D increases, v increases, E curve is asymptotic
    to OA
  • Shooting flow
  • D decreases, v increases, E curve will be
    asymptotic to the E axis.

25
  • Which of the two alternate depths for a given E
    will occur at a cross section depends on the
    slope of the channel.
  • Critical slope, sc, is defined as the slope of
    the channel which will maintain flow at critical
    depth, DC.
  • Uniform tranquil s lt sc mild slope
  • Uniform shooting flow s gt sc steep slope

26
Example 4.1
  • A rectangular channel 8 m wide conveys water at
    a rate of 15 m3/s. If the velocity in the channel
    is 1.5 m/s, determine
  • a) E
  • b) DC
  • c) vc
  • d) Emin
  • e) Type of flow

27
Example 4.2
  • Determine the critical depth in the trapezoidal
    channel shown below if the discharge in the
    channel is 0.34 m3/s. The channel has side slopes
    with a vertical to horizontal ratio of 11.

28
Example 4.3
  • Determine the critical depth in a channel of
    triangular cross section conveying water at a
    velocity of 2.75 m/s and at a depth of 1.25 m.
    The channel has side slopes of 12.

29
Exercise
  • A channel has a trapezoidal cross-section with a
    base width of 0.6 m and sides sloping at 450.
    When the flow along the channel is 20 m3 min-1,
    determine the critical depth. (0.27 m)

30
Control sections
  • Control sections cross sections at which the
    flow passes through the critical depth.
  • Such sections are limiting factor in the design
    of channel. and some of the cases in which they
    occur are
  • Transition from tranquil to shooting flow
  • Entrance to a channel of steep slope from a
    reservoir
  • Free outfall from a channel with a mild slope
  • Change in bed level or change in width of channel

31
Transition from tranquil to shooting flow
32
  • May occur where there is a change of bed slope s.
  • Upstream slope is mild and s is less than the
    critical slope sc.
  • Over s considerable distance the depth will
    change smoothly from D1 to D2.
  • At the break in the slope, the depth will pass
    through DC forming a control section which
    regulates the upstream depth.
  • At the tail end, the reverse transition from
    shooting to tranquil flow occurs suddenly by
    means of a hydraulic jump.

33
Entrance to a channel of steep slope from a
reservoir
  • If depth of flow in the channel is less than DC
    for the channel, water surface must pass through
    DC in the vicinity of the entrance, since
    conditions in the reservoir correspond to
    tranquil flow.

34
Free Outfall from a Channel with a Mild Slope
35
  • If slope s of the channel is less than sc the
    upstream flow will be tranquil.
  • At the outfall, theoretically, the depth will be
    critical, DC.
  • In practice, gravitational acceleration will
    cause an increase of velocity at the brink so
    that D lt DC.
  • While experiments indicate that depending on the
    slope upstream
  • DC occurs at distance of between 3DC to 10DC from
    the brink.
  • D at the brink is approximately 0.7DC.

36
(No Transcript)
37
Flow over a broad-crested weir
  • Broad-crested weir is an obstruction in the form
    of a raised portion of the bed extending across
    the full width of the channel with a flat upper
    surface or crest sufficiently broad in the
    direction of flow for the surface of the liquid
    to become parallel to the crest.
  • Upstream edge is rounded to avoid separation
    losses that occur at a sharp edged.
  • The flow upstream of the weir is tranquil and the
    conditions downstream of the weir allow a free
    fall over the weir.

38
(No Transcript)
39
  • The discharge over the weir will be, therefore,
    be the maximum possible and flow over the weir
    will take place at DC.
  • For a rectangular channel,
  • (16.11)

40
  • The specific energy, E, measured above the crest
    of the weir will be (assuming no losses),
  • H is the height of the upstream water level
    above the crest and v is the mean velocity at a
    point upstream where flow is uniform.
  • If the upstream depth is large compared with the
    depth over the weir, (v2/2g) is negligible,
    therefore,
  • Rewriting (16.11),
  • (16.12)

41
  • A single measurement of the head, H above the
    crest of the weir would then be sufficient to
    determine Q.
  • Since , the depth over the crest
    of the weir is fixed, irrespective of its height.
  • Any increase in the weir height will not change
    DC but will cause an increase in the depth of the
    flow upstream.
  • Therefore, maximum height of the weir,

42
  • If the level of the flow downstream is raised,
    the surface level will be drawn down over the
    hump, but the depth may not fall to the critical
    depth.
  • The rate of flow can be calculated by applying
    Bernoullis s Equation and continuity equation
    and depends on the difference in surface level
    upstream and over the weir.

43
Example 4.4
  • A broad crested weir 500 mm high is used to
    measure the discharge in a rectangular channel.
    The width of the channel is 20 m and the height
    of the channel upstream of the weir is 1.25 m.
    What is the discharge in the channel if water
    falls freely over the weir? Assume that the
    velocity upstream is very small. Determine the
    difference in water level between upstream and
    over the top of the weir.

44
Effect of lateral contraction of a channel
  • When width of a channel is reduced while bed
    remains flat, q increases.
  • As channel narrows - neglecting losses, E remains
    constant for tranquil flow, depth will decrease
    while for shooting flow depth will increases.

45
(No Transcript)
46
Free surface does not pass through DC
47
  • Arrangement forms a venturi flume (venturi
    meter).
  • Applying energy equation between upstream
    throat and ignoring losses,

48
  • Actual discharge,
  • Cd is a coefficient of discharge 0.95 to 0.99

49
Free surface passes through DC
50
  • The flowrate is given by,
  • Assuming that the upstream velocity head is
    negligible,
  • (16.15)
  • where H is the of the upstream free surface
    above bed level at the throat.

51
Lateral contraction with hump
52
  • Height of upstream water level above the hump, H
    D1 Z
  • When upstream conditions are tranquil and the bed
    slope is the same downstream as upstream,
    impossible for shooting flow to be maintained for
    any great distance from the throat.
  • Revert to tranquil flow downstream by means of a
    hydraulic jump or standing wave.
  • Venturi flume operating in this mode is known as
    standing wave flume.

53
Example 4.5
  • A venturi flume is constructed in a channel
    which is 3.5 m wide. If the throat width in the
    flume is 1.2 m and the depth upstream from the
    constriction is 1.25 m , calculate the discharge
    in the channel when the depth at the throat is
    1.2 m. If the conditions are such that a standing
    wave is formed, what is the discharge?

54
Example 4.6
  • A Venturi flume is 2.5m wide and 1.4m deep
    upstream with a throat width of 1.3m. Assuming
    that a standing wave form downstream, calculate
    the rate of flow of water if the discharge
    coefficient is 0.94. Do not ignore the velocity
    of approach.

55
Review of past semesters questions
56
APR 2010
  • A 10 m wide channel conveys 25 m3/s of water at a
    depth of 1.6 m. Determine
  • i) specific energy of the flowing water
  • ii) critical depth, critical velocity and
    minimum specific energy

57
APR 2010
  • A venturi flume is 1.40 m wide at the entrance
    and 0.7 m wide at the throat. Determine the flow
    if the depths at the entrance and at the throat
    is 0.8 m and 0.6 m respectively. Neglect all
    losses.
Write a Comment
User Comments (0)
About PowerShow.com