Download presentation

1
**Fluid Mechanics 2 The Bernoulli Equation**

CEVE 101 Fluid Mechanics 2 The Bernoulli Equation Dr. Phil Bedient

2
**FLUID DYNAMICS THE BERNOULLI EQUATION**

The laws of Statics that we have learned cannot solve Dynamic Problems. There is no way to solve for the flow rate, or Q. Therefore, we need a new dynamic approach to Fluid Mechanics.

3
**The Bernoulli Equation**

By assuming that fluid motion is governed only by pressure and gravity forces, applying Newton’s second law, F = ma, leads us to the Bernoulli Equation. P/g + V2/2g + z = constant along a streamline (P=pressure g =specific weight V=velocity g=gravity z=elevation) A streamline is the path of one particle of water. Therefore, at any two points along a streamline, the Bernoulli equation can be applied and, using a set of engineering assumptions, unknown flows and pressures can easily be solved for.

4
**The Bernoulli Equation (unit of L)**

At any two points on a streamline: P1/g + V12/2g + z1 = P2/g + V22/2g + z2 1 2

5
**Determine the difference in pressure between points 1 and 2**

A Simple Bernoulli Example V2 Z g = gair Determine the difference in pressure between points 1 and 2 Assume a coordinate system fixed to the bike (from this system, the bicycle is stationary, and the world moves past it). Therefore, the air is moving at the speed of the bicycle. Thus, V2 = Velocity of the Biker Hint: Point 1 is called a stagnation point, because the air particle along that streamline, when it hits the biker’s face, has a zero velocity (see next slide)

6
Stagnation Points On any body in a flowing fluid, there is a stagnation point. Some fluid flows over and some under the body. The dividing line (the stagnation streamline) terminates at the stagnation point. The Velocity decreases as the fluid approaches the stagnation point. The pressure at the stagnation point is the pressure obtained when a flowing fluid is decelerated to zero speed by a frictionless process

7
**Apply Bernoulli from 1 to 2**

V2 Z g = gair Point 1 = Point 2 P1/gair + V12/2g + z1 = P2/gair + V22/2g + z2 Knowing the z1 = z2 and that V1= 0, we can simplify the equation P1/gair = P2/gair + V22/2g P1 – P2 = ( V22/2g ) gair

8
**A Simple Bernoulli Example**

If Lance Armstrong is traveling at 20 ft/s, what pressure does he feel on his face if the gair= lbs/ft3? We can assume P2 = 0 because it is only atmospheric pressure P1 = ( V22/2g )(gair) = P1 = ((20 ft/s)2/(2(32.2 ft/s2)) x lbs/ft3 P1 =.475 lbs/ft2 Converting to lbs/in2 (psi) P1 = psi (gage pressure) If the biker’s face has a surface area of 60 inches He feels a force of x 60 = .198 lbs

9
**Bernoulli Assumptions**

There are three main variables in the Bernoulli Equation Pressure – Velocity – Elevation To simplify problems, assumptions are often made to eliminate one or more variables Key Assumption # 1 Velocity = 0 Imagine a swimming pool with a small 1 cm hole on the floor of the pool. If you apply the Bernoulli equation at the surface, and at the hole, we assume that the volume exiting through the hole is trivial compared to the total volume of the pool, and therefore the Velocity of a water particle at the surface can be assumed to be zero

10
**Bernoulli Assumptions**

Key Assumption # 2 Pressure = 0 Whenever the only pressure acting on a point is the standard atmospheric pressure, then the pressure at that point can be assumed to be zero because every point in the system is subject to that same pressure. Therefore, for any free surface or free jet, pressure at that point can be assumed to be zero.

11
**The Continuity Equation**

Bernoulli Assumptions Key Assumption # 3 The Continuity Equation In cases where one or both of the previous assumptions do not apply, then we might need to use the continuity equation to solve the problem A1V1=A2V2 Which satisfies that inflow and outflow are equal at any section

12
**Bernoulli Example Problem: Free Jets**

What is the Flow Rate at point 2? What is the velocity at point 3? Givens and Assumptions: Because the tank is so large, we assume V1 = 0 (Volout <<< Voltank) The tank is open at both ends, thus P1 = P2 = P3 = atm P1 and P2 and P3= 0 Part 1: Apply Bernoulli’s eqn between points 1 and 2 P1/gH2O + V12/2g + h = P2/gH20 + V22/2g + 0 simplifies to h = V22/2g solving for V V = √(2gh) Q = VA or Q = A2√(2gh) 1 γH2O 2 A2 3

13
**Bernoulli Example Problem: Free Jets**

Part 2: Find V3? Apply Bernoulli’s eq from pt 1 to pt 3 P1/gH2O + V12/2g + h = P3/gH20 + V32/2g – H Simplify to h + H = V32/2g Solving for V V3 = √( 2g ( h + H )) 1 γH2O 2 Z = 0 A2 3

14
**The Continuity Equation**

Why does a hose with a nozzle shoot water further? Conservation of Mass: In a confined system, all of the mass that enters the system, must also exit the system at the same time. Flow rate = Q = Area x Velocity r1A1V1(mass inflow rate) = r2A2V2( mass outflow rate) If the fluid at both points is the same, then the density drops out, and you get the continuity equation: A1V1 =A2V2 Therefore If A2 < A1 then V2 > V1 Thus, water exiting a nozzle has a higher velocity V1 -> A1 A2 V2 -> Q2 = A2V2 Q1 = A1V1 A1V1 = A2V2

15
Free Jets The velocity of a jet of water is clearly related to the depth of water above the hole. The greater the depth, the higher the velocity. Similar behavior can be seen as water flows at a very high velocity from the reservoir behind a large dam such as Hoover Dam

16
**The Energy Line and the Hydraulic Grade Line**

Looking at the Bernoulli equation again: P/g + V2/2g + z = constant on a streamline This constant is called the total head (energy), H Because energy is assumed to be conserved, at any point along the streamline, the total head is always constant Each term in the Bernoulli equation is a type of head. P/g = Pressure Head V2/2g = Velocity Head Z = elevation head These three heads summed equals H = total energy Next we will look at this graphically…

17
**The Energy Line and the Hydraulic Grade Line**

Measures the static pressure Pitot measures the total head 1: Static Pressure Tap Measures the sum of the elevation head and the pressure Head. 2: Pitot Tube Measures the Total Head EL : Energy Line Total Head along a system HGL : Hydraulic Grade line Sum of the elevation and the pressure heads along a system 1 2 EL V2/2g HGL Q P/g Z

18
**The Energy Line and the Hydraulic Grade Line**

Understanding the graphical approach of Energy Line and the Hydraulic Grade line is key to understanding what forces are supplying the energy that water holds. Point 1: Majority of energy stored in the water is in the Pressure Head Point 2: Majority of energy stored in the water is in the elevation head If the tube was symmetrical, then the velocity would be constant, and the HGL would be level EL V2/2g V2/2g HGL P/g 2 Q P/ g Z 1 Z

19
Tank Example Solve for the Pressure Head, Velocity Head, and Elevation Head at each point, and then plot the Energy Line and the Hydraulic Grade Line Assumptions and Hints: P1 and P4 = V3 = V4 same diameter tube We must work backwards to solve this problem 1 R = .5’ 4’ R = .25’ 2 3 4 1’

20
**Pressure Head : Only atmospheric P1/g = 0 **

Point 1: Pressure Head : Only atmospheric P1/g = 0 Velocity Head : In a large tank, V1 = 0 V12/2g = 0 Elevation Head : Z1 = 4’ 1 4’ R = .5’ R = .25’ 2 3 4 1’

21
**Pressure Head : Only atmospheric P4/ g = 0**

Point 4: Apply the Bernoulli equation between 1 and = 0 + V42/2(32.2) + 1 V4 = 13.9 ft/s Pressure Head : Only atmospheric P4/ g = 0 Velocity Head : V42/2g = 3’ Elevation Head : Z4 = 1’ 1 γH2O= 62.4 lbs/ft3 4’ R = .5’ R = .25’ 2 3 4 1’

22
Point 3: Apply the Bernoulli equation between 3 and 4 (V3=V4) P3/ = P3 = 0 Pressure Head : P3/g = 0 Velocity Head : V32/2g = 3’ Elevation Head : Z3 = 1’ 1 4’ R = .5’ R = .25’ 2 3 4 1’

23
**Apply the Continuity Equation**

Point 2: Apply the Bernoulli equation between 2 and P2/ V22/2(32.2) + 1 = Apply the Continuity Equation (P.52)V2 = (P.252)x13.9 V2 = ft/s P2/ /2(32.2) + 1 = 4 P2 = lbs/ft2 Pressure Head : P2/ g = 2.81’ Velocity Head : V22/2g = .19’ Elevation Head : Z2 = 1’ 1 4’ R = .5’ R = .25’ 2 3 4 1’

24
Plotting the EL and HGL Energy Line = Sum of the Pressure, Velocity and Elevation heads Hydraulic Grade Line = Sum of the Pressure and Velocity heads V2/2g=.19’ EL P/ g =2.81’ V2/2g=3’ V2/2g=3’ Z=4’ HGL Z=1’ Z=1’ Z=1’

25
**Pipe Flow and Open Channel Flow**

CEVE 101 Pipe Flow and Open Channel Flow

26
Open Channel Flow Uniform Open Channel Flow is the hydraulic condition in which the water depth and the channel cross section do not change over some reach of the channel Manning’s Equation was developed to relate flow and channel geometry to water depth. Knowing Q in a channel, one can solve for the water depth Y. Knowing the maximum allowable depth Y, one can solve for Q.

27
Open Channel Flow Manning’s equation is only accurate for cases where the cross sections of a stream or channel are uniform. Manning’s equation works accurately for man made channels, but for natural streams and rivers, it can only be used as an approximation.

28
**Manning’s Equation Terms in the Manning’s equation:**

V = Channel Velocity A = Cross sectional area of the channel P = Wetted perimeter of the channel R = Hydraulic Radius = A/P S = Slope of the channel bottom (ft/ft or m/m) n = Manning’s roughness coefficient (.015, .045, .12) Yn = Normal depth (depth of uniform flow) Area Yn Y X Wetted Perimeter Slope = S = Y/X

29
**For a rectangular Channel**

Manning’s Equation V = (1/n)R2/3√(S) for the metric system V = (1.49/n)R2/3√(S) for the English system Q = A(k/n)R2/3√(S) k is either 1 or 1.49 Yn is not directly a part of Manning’s equation. However, A and R depend on Yn. Therefore, the first step to solving any Manning’s equation problem, is to solve for the geometry’s cross sectional area and wetted perimeter: For a rectangular Channel Area = A = B x Yn Wetted Perimeter = P = B + 2Yn Hydraulic Radius = A/P = R = BYn/(B+2Yn) Yn B

30
**Simple Manning’s Example Next, apply Manning’s equation**

A rectangular open concrete (n=0.015) channel is to be designed to carry a flow of 2.28 m3/s. The slope is m/m and the bottom width of the channel is 2 meters Determine the normal depth that will occur in this channel. First, find A, P and R A = 2Yn P = 2 + 2Yn R = 2Yn/(2 + 2Yn) Next, apply Manning’s equation Q = A(1/n)R2/3√(S) 2.28 = (2Yn)x(1/0.015) * (2Yn/(2 + 2Yn))2/3 * √(0.006) Solving for Yn with Goal Seek Yn = 0.47 meters Yn 2 m

31
**The Trapezoidal Channel**

House flooding occurs along Brays Bayou when water overtops the banks. What flow is allowable in Brays Bayou if it has the geometry shown below? Slope S = ft/ft 25’ a = 20° Concrete Lined n = 0.015 B=35’ A, P and R for Trapezoidal Channels A = Yn(B + Yn cot a) P = B + (2Yn/sin a ) R = (Yn(B + Yn cot a)) / (B + (2Yn/sin a)) Yn θ B

32
**The Trapezoidal Channel**

Slope S = ft/ft 25’ Θ = 20° Concrete Lined n = 0.015 35’ A = Yn(B + Yn cot a) A = 25( cot(20)) = 2592 ft2 P = B + (2Yn/sin a ) P = 35 + (2 x 25/sin(20)) = ft R = 2592’ / 181.2’ = 14.3 ft

33
**The Trapezoidal Channel**

Slope S = ft/ft 25’ Θ = 20° Concrete Lined n = 0.015 35’ Q for Bayou = A(1.49/n)R2/3√(S) Q = 2592 x (1.49 / .015) (14.3)2/3 √(.0003) Q = Max allowable Flow = 26,300 cfs

34
**Manning’s Over Different Terrains**

S = .005 ft/ft 5’ 5’ 5’ 3’ 3’ Grass n=.03 Grass n=.03 Concrete n=.015 Estimate the flow rate for the above channel? Hint: Treat each different portion of the channel separately. You must find an A, R, P and Q for each section of the channel that has a different n coefficient. Neglect dotted line segments.

35
**Manning’s Over Grass The Grassy portions:**

S = .005 ft/ft 5’ 5’ 5’ 3’ 3’ Grass n=.03 Grass n=.03 Concrete n=.015 The Grassy portions: For each section: A = 5’ x 3’ = 15 ft2 P = 5’ + 3’ = 8 ft R = 15 ft2/8 ft = 1.88 ft Q = 15(1.49/.03)1.882/3√(.005) Q = cfs per section For both sections… Q = 2 x = cfs

36
**Manning’s Over Concrete**

S = .005 ft/ft 5’ 5’ 5’ 3’ 3’ Grass n=.03 Grass n=.03 Concrete n=.015 The Concrete section A = 5’ x 6’ = 30 ft2 P = 5’ + 3’ + 3’= 11 ft R = 30 ft2/11 ft = 2.72 ft Q = 30(1.49/.015)2.722/3√(.005) Q = cfs For the entire channel… Q = = 540 cfs

37
**Pipe Flow and the Energy Equation**

For pipe flow, the Bernoulli equation alone is not sufficient. Friction loss along the pipe, and momentum loss through diameter changes and corners take head (energy) out of a system that theoretically conserves energy. Therefore, to correctly calculate the flow and pressures in pipe systems, the Bernoulli Equation must be modified. P1/g + V12/2g + z1 = P2/g + V22/2g + z2 + Hmaj + Hmin Energy line with no losses Hmaj Energy line with major losses 1 2

38
Major Losses Major losses occur over the entire pipe, as the friction of the fluid over the pipe walls removes energy from the system. Each type of pipe as a friction factor, f, associated with it. Hmaj = f (L/D)(V2/2g) Energy line with no losses Hmaj Energy line with major losses 1 2

39
Minor Losses Unlike major losses, minor losses do not occur over the length of the pipe, but only at points of momentum loss. Since Minor losses occur at unique points along a pipe, to find the total minor loss throughout a pipe, sum all of the minor losses along the pipe. Each type of bend, or narrowing has a loss coefficient, KL to go with it. Minor Losses

40
**Major and Minor Losses Major Losses: Minor Losses:**

Hmaj = f (L/D)(V2/2g) f = friction factor L = pipe length D = pipe diameter V = Velocity g = gravity Minor Losses: Hmin = KL(V2/2g) Kl = sum of loss coefficients V = Velocity g = gravity When solving problems, the loss terms are added to the system at the second analysis point P1/g + V12/2g + z1 = P2/g + V22/2g + z2 + Hmaj + Hmin

41
Loss Coefficients

42
**Pipe Flow Example goil= 8.82 kN/m3**

1 Z1 = ? 2 Z2 = 130 m 60 m Kout=1 7 m r/D = 0 130 m r/D = 2 If oil flows from the upper to lower reservoir at a velocity of 1.58 m/s in the D= 15 cm smooth pipe, what is the elevation of the oil surface in the upper reservoir? Include major losses along the pipe, and the minor losses associated with the entrance, the two bends, and the outlet.

43
**Hmaj = (f L V2)/(D 2g)=(.035 x 197m * (1.58m/s)2)/(.15 x 2 x 9.8m/s2)**

Pipe Flow Example 1 Z1 = ? 2 Z2 = 130 m 60 m Kout=1 7 m r/D = 0 130 m r/D = 2 Apply Bernoulli’s equation between points 1 and 2: Assumptions: P1 = P2 = Atmospheric = V1 = V2 = 0 (large tank) Z1 = m + Hmaj + Hmin Hmaj = (f L V2)/(D 2g)=(.035 x 197m * (1.58m/s)2)/(.15 x 2 x 9.8m/s2) Hmaj= 5.85m

44
**Pipe Flow Example 0 + 0 + Z1 = 0 + 0 + 130m + 5.85m + Hmin**

2 Z2 = 130 m 60 m Kout=1 7 m r/D = 0 130 m r/D = 2 Z1 = m m + Hmin Hmin= 2KbendV2/2g + KentV2/2g + KoutV2/2g From Loss Coefficient table: Kbend = Kent = Kout = 1 Hmin = (0.19x ) * (1.582/2*9.8) Hmin = 0.24 m

45
**Pipe Flow Example 0 + 0 + Z1 = 0 + 0 + 130m + 5.85m + 0.24m**

Kout=1 7 m r/D = 0 130 m r/D = 2 Z1 = m + Hmaj + Hmin Z1 = m m m Z1 = meters

46
**Stormwater Mgt Model (SWWM)**

Most advanced model ever written for dynamic hydraulic routing Solves complex equations for pipe flow with consideration of tailwater at outlet New graphical user interface for easy input and presentation of results Will allow for direct evaluation of flood control options under various conditions

47
**SWMM Input Rainfall Pattern Inlets to Pipes Pipe Elevations and Sizes**

Junction Locations Bayou Level

48
**SWMM Output Flooding Areas High Bayou Level Pipe at Capacity**

Backflow at Outlet

Similar presentations

Presentation is loading. Please wait....

OK

Pertemuan CLOSED CONDUIT FLOW 1

Pertemuan CLOSED CONDUIT FLOW 1

© 2018 SlidePlayer.com Inc.

All rights reserved.

Ads by Google

View my ppt online student Ppt on natural disasters in india Ppt on event handling in javascript output Ppt on brand marketing jobs Ppt on employee motivation and job satisfaction Ppt on conservation of forest in india Ppt on use of maths in our daily life Ppt on pre ignition causes Ppt on types of parallelograms quadrilateral Ppt on centring meditation