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Module 6

Lecture 5: equation and numerical problems Energy in Gradually Varied Open channel flow

 In a closed conduit there can be a pressure gradient that drives the flow.  An open channel has atmospheric pressure at the surface.  The HGL (Hydraulic Gradient Line) is thus the same as the fluid surface.

Module 6 Energy equation applied to open channel

p v 2 p v 2 1 + α 1 + z = 2 + α 2 + z + h γ 1 2g 1 γ 2 2g 2 L

p1 and p2 : pressure forces per unit width at sections 1 & 2 respectively v1 and v2 : velocity of flow at sections 1 & 2 respectively α α1 and 2 : energy coefficients z1 and z2: elevations of channel bottom at sections 1 & 2 respectively w.r.t any datum hL: energy head loss of flow through the channel

Module 6 Energy equation applied to open channel Contd…

Simplifications made to the Energy Equation: 1. Assume turbulent flow (α = 1).

2. Assume the slope is zero locally, so that z1 = z2 3. Write pressure in terms of depth (y = p / γ).

4. Assume friction is negligible (hL = 0).

i.e. v 2 v 2 y + 1 = y + 2 1 2g 2 2g

E1 = E2

Module 6 Specific Energy Equation

Energy at a particular point in the channel = +

2 E = y + v 2g or Q 2 E = y + 2 2gA where y is the depth of flow, v is the velocity, Q is the discharge, A is the cross- sectional flow area and E is the specific energy i.e energy w.r.t channel bottom.

Module 6 Total energy

 When energy is measured with respect to another fixed datum , it’s called Total Energy 2 E = y + z + v 2g

where z is the height of the channel bottom from the datum

 Pressure head (y) is the ratio of pressure and the specific weight of

 Elevation head or the datum head (z) is the height of the section under consideration above a datum

 Velocity head (v2/2g) is due to the average velocity of flow in that vertical section Module 6 Example Problem

Channel width (rectangular) = 2m, Depth = 1m, Q = 3.0 m3/s, Height above datum = 2m. Compute specific and total energy

Ans: A = b*y = 2.0*1.0 = 2 m2

Q 2 E = y + 2 Specific energy = 2gA

32 Total energy = E = 1+ 2 2*9.81* 2

Datum height + specific energy = 2.0 + 1.20 = 3.20 m

Module 6 Specific Energy Diagram

The specific energy can be plotted graphically as a function of depth of flow : E = Es + Ek where Q 2 E = y + 2 2gA

Es = y (Static energy) Q 2 E = 2 (Kinetic energy) k 2gA Module 6 Specific Energy Diagram Contd…

Module 6 Specific Energy Diagram Contd…

As the depth of flow increases, the static energy increases and the kinetic energy decreases,

y ∞ Es ⇒ y ∞ 1 Ek

The total energy curve approaches the static energy curve for high depths and the kinetic energy curve for small depths As discharge (Q) increases, the specific energy curves move to the upper right portion of the graph

Module 6 Thus, for flat slope (+ other assumptions…) we can graph y against E: (Recall for given flow, E1 = E2 )

Curve for different, higher Q.

For given Q and E, usually have 2 allowed depths: Subcritical and supercritical flow.

Module 6 The specific energy is minimum (Emin) for a particular  critical depth – Depth Froude’s number = 1.0. & velocity = Vc. Emin  only energy value with a singular depth! Depths < critical depths – supercritical flow (Calm, tranquil flow) Froude Number > 1.0. V > Vc. Depths > critical depths – subcritical flow (Rapid flow, “whitewater”) Froude Number < 1.0. V < Vc. Example: Flow past a sluice gate

Module 6 Critical Depth and Froude Number

At the turning point (the left-most point of the blue curve), there is just one value of y(E).

This point can be found from

It can easily be shown that at ,

Module 6 Critical Depth and Froude Number Contd…

The Froude number can be defined as:

(Recall that the Reynolds number is the ratio of acceleration to viscous forces). The Froude number is the ratio of acceleration to gravity Perhaps more illustrative is the fact that surface (gravity) waves move at a speed of

Flows with Fr < 1 move slower than gravity waves. Flows with Fr > 1 move faster than gravity waves. Flows with Fr = 1 move at the same speed as gravity waves.

Module 6 Critical Depth and Froude Number Contd…

Flows sometimes switch from supercritical to subcritical:

(The switch depends on upstream and downstream velocities)

Gravity waves: If you throw a rock into the water, the entire circular wave will travel downstream in supercritical flow.

In subcritical flow, the part of the wave trying to travel upstream will in fact move upstream (against the flow of the current).

Module 6 Example Problem

Will the flow over a bump be supercritical or subcritical?

Left Right

Left Right or

As it turns out: Left = subcritical Right = supercritical

Using the Bernoulli equation for frictionless, steady, incompressible flow along a streamline:

Module 6 Example Problem Contd…

Apply Bernoulli equation along free surface streamline (p=0):

For a channel of rectangular cross-section,

Module 6 Example Problem Contd…

Substitute Q = V z b into Bernoulli equation:

To find the shape of the free surface, take the x-derivative:

Solve for dz / dx:

Module 6 Example Problem Contd…

Since subcritical: Fr < 1 supercritical: Fr > 1

Subcritical flow with dh / dx > 1 dz / dx < 1 Supercritical flow with dh / dx > 1 dz / dx > 1

if flow is subcritical if flow is supercritical

Module 6 Hydraulic Jump

Module 6 Hydraulic Jump Contd…

There is a lot of viscous dissipation ( = head loss ) within the hydraulic jump.

Module 6 Hydraulic Jump Contd…

Apply the momentum equation:

Momentum equation is used here as there is an unknown loss of energy (where mechanical energy is converted to ). But as long as there is no friction along the base of the flow, there is no loss of momentum involved.

Module 6 Hydraulic Jump Contd…

Momentum balance: The forces are hydrostatic forces on each end:

(where and are the pressures at centroids of A1 and A2 ) Module 6 Hydraulic Jump Contd…

If y1 and Q are given, then for rectangular channel

is the pressure at mid-depth.

Here, entire left-hand side is known, and we also know the first term on the

right-hand side. So we can find V2.

Module 6 Exercises

1) A rectangular channel 4m wide has a flow discharge of 10.0 m3/s and depth of flow as 2.5 m. Draw specific energy diagram and find critical and alternate depth. 2) A triangular channel with side slopes having ratio of 1:1.5 has a discharge capacity of 0.02 m3/s. Calculate: a. critical depth b. Emin c. Plot specific energy curve d. Determine energy for 0.25 ft and alternate depth e. Velocity of flow and Froude number f. Calculate required slopes if depths from d are to be normal depths for given flow. Module 6 Highlights in the Module

 Reynolds' transport theorem (Leibniz-Reynolds' transport theorem) is a 3- D generalization of the Leibniz integral rule.

 Control volume is a definite volume specified in space. Matter in a control volume can change with time as matter enters and leaves its control surface.

 Reynolds Transport Theorem states that the total rate of change of any extensive property B of a system occupying a control volume C.V. at time ‘t’ is equal to the sum of: a) the temporal rate of change of B within the C.V. b) the net flux of B through the control surface C.S. that surrounds the C.V.

Module 6 Highlights in the Module Contd…

 St.Venant equations are derived from Navier-Stokes Equations for shallow water flow conditions.  The solution of the St. Venant equations is known as dynamic routing, which is generally the standard to which other methods are measured or compared.

 Forces acting on the C.V. in an open channel flow are gravity force, friction force , contraction/expansion force, wind shear force and unbalanced pressure forces.

 Solutions to St. Venant equations :  Method of characteristics  Finite Difference methods : Explicit, Implicit  Finite Element Methods

Module 6