CHAPTER 1. Problem 1: (a) Trapezoidal channel with side slopes m 1 and m 2 y y

Similar documents
Hydraulic jump (lab. scale)

Experiment 7 Energy Loss in a Hydraulic Jump

Water Flow in Open Channels

OPEN CHANNEL FLOW. One-dimensional - neglect vertical and lateral variations in velocity. In other words, Q v = (1) A. Figure 1. One-dimensional Flow

3.2 CRITICAL DEPTH IN NONRECTANGULAR CHANNELS AND OCCUR- RENCE OF CRITICAL DEPTH

NOTES ON OPEN CHANNEL FLOW

VARIED FLOW IN OPEN CHANNELS

Local energy losses at positive and negative steps in subcritical open channel flows

LECTURE NOTES - III. Prof. Dr. Atıl BULU

APPENDIX A. Watershed Delineation and Stream Network Defined from WMS

Open Channel Flow I - The Manning Equation and Uniform Flow COURSE CONTENT

SOLID AND FLUID MECHANICS CPE LEVEL I TRAINING MODULE

Kolmetz Handbook Process Equipment Design SOLID AND FLUID MECHANICS (ENGINEERING FUNDAMENTALS)

Chapter 2 Basic Conservation Equations for Laminar Convection

Energy transfer rates in turbulent channels with drag reduction at constant power input

Bubble curtain system for prevention of seawater intrusion in coastal aquifers

Cumulative Review of Vectors

Uniform Channel Flow Basic Concepts. Definition of Uniform Flow

SOLUTION y ' A = 7.5(15) (150) + 90(150) (15) + 215(p)(50) 2. = mm 2. A = 15(150) + 150(15) + p(50) 2. =

Properties and Definitions Useful constants, properties, and conversions

F = 0 can't be satisfied.

Open Channel Hydraulics I - Uniform Flow

Hydraulics Part: Open Channel Flow

Hydromechanics: Course Summary

Basic Hydraulics. Rabi H. Mohtar ABE 325

Conservation of Linear Momentum for a Differential Control Volume

Second Moments or Moments of Inertia

Numerical Analysis of Heat Transfer in the Unsteady Flow of a non- Newtonian Fluid over a Rotating cylinder

Chapter 4: Non uniform flow in open channels

Geomorphology 5. Stream Sediment Stream Sediment

Prof. B.S. Thandaveswara. A short horizontal reach of a prismatic channel is considered. Further, the external

HKIE-GD Workshop on Foundation Engineering 7 May Shallow Foundations. Dr Limin Zhang Hong Kong University of Science and Technology

Method of Images

LECTURE 9: Open channel flow: Uniform flow, best hydraulic sections, energy principles, Froude number

M E 320 Professor John M. Cimbala Lecture 38

Sourabh V. Apte. 308 Rogers Hall

EXPERIMENTAL STUDY OF BACKWATER RISE DUE TO BRIDGE PIERS AS FLOW OBSTRUCTIONS

ME 141. Lecture 8: Moment of Inertia

CHAPTER 4 The Integral Forms of the Fundamental Laws

Characteristics of flow over the free overfall of triangular channel

We will assume straight channels with simple geometries (prismatic channels) and steady state flow (in time).

Q = α n AR2/3 h S1/2 0. bd 2d + b d if b d. 0 = ft1/3 /s

FLUID MECHANICS. 1. Division of Fluid Mechanics. Hydrostatics Aerostatics Hydrodynamics Gasdynamics. v velocity p pressure ρ density

PHY4116 From Newton to Einstein. Mid-Term Test, 10a.m. Wed. 16 th Nov Duration: 50 minutes. There are 25 marks in Section A and 25 in Section B.

Stress-strain relations

I xx + I yy + I zz = (y 2 + z 2 )dm + (x 2 + y 2 )dm. (x 2 + z 2 )dm + (x 2 + y 2 + z 2 )dm = 2

ACCOUNTING FOR FRICTION IN THE BERNOULLI EQUATION FOR FLOW THROUGH PIPES

Presented by: Civil Engineering Academy

Chapter 3.8: Energy Dissipators. By Dr. Nuray Denli Tokyay

Fluid Mechanics II. Newton s second law applied to a control volume

Geology 550 Spring 2005 LAB 3: HYDRAULICS OF PRAIRIE CREEK

Distributed Forces: Moments of Inertia

Pressure Head: Pressure head is the height of a column of water that would exert a unit pressure equal to the pressure of the water.

Design Data 17. Partial Flow Conditions of Box Culverts

What about water... What about open channel flow... Continuity Equation. HECRAS Basic Principles of Water Surface Profile Computations

CONSERVATION OF ENERGY FOR ACONTINUUM

Electricity & Magnetism Lecture 13

Conveyance Estimation System (CES) Launch

Chapter 6 The Impulse-Momentum Principle

1. Open Channel Hydraulics

Note: Referred equations are from your textbook.

Hydrology & Irrigation. Civil Engineering

PUMP SYSTEM ANALYSIS AND SIZING. BY JACQUES CHAURETTE p. eng.

15. Physics of Sediment Transport William Wilcock

DIMENSIONAL ANALYSIS IN MOMENTUM TRANSFER

LECTURE NOTES - VIII. Prof. Dr. Atıl BULU

Formation Of Hydraulic Jumps On Corrugated Beds

Math 122 Fall Solutions to Homework #5. ( ) 2 " ln x. y = x 2

FORMATION OF HYDRAULIC JUMPS ON CORRUGATED BEDS

S O A O lllllu O, W E D N E S D A Y N E X T ; D E C 2 9 t h. R E D U C T I O N S. 3 1, 3 2, 3 3, R o b e r t s o n S t., 2 & 3 Q a r e m o n t,

7. TURBULENCE SPRING 2019

MATHEMATICS, NUMERICS, DERIVATIONS AND OPENFOAM

STATICS. Moments of Inertia VECTOR MECHANICS FOR ENGINEERS: Ninth Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr.

ECOHYDRAULICS. Introduction to 2D Modeling

CIE4491 Lecture. Hydraulic design

Chapter 18 KINETICS OF RIGID BODIES IN THREE DIMENSIONS. The two fundamental equations for the motion of a system of particles .

A Simple Turbulence Closure Model. Atmospheric Sciences 6150

USHA RAMA COLLEGE OF ENGINEERING & TECHNOLOGY

Units and Dimensions. Lecture 1. Introduction to Chemical Engineering Calculations

Thermodynamics System Surrounding Boundary State, Property Process Quasi Actual Equilibrium English

UNIVERSITY OF OSLO. Faculty of Mathematics and Natural Sciences. MEK4300/9300 Viscous flow og turbulence

A Simple Turbulence Closure Model

Lecture Notes - Sediment Transport The flow problem Overview

Request for bridge scour analysis for complex pier foundations

39.1 Gradually Varied Unsteady Flow

INSTRUCTIONS TO CANDIDATES:

Numerical Hydraulics

CEE 3310 Open Channel Flow, Nov. 26,

Physics 201 Lecture 29

STRESSES IN SOIL MASS

ENGR 292 Fluids and Thermodynamics

STATICS. Moments of Inertia VECTOR MECHANICS FOR ENGINEERS: Seventh Edition CHAPTER. Ferdinand P. Beer

Symmetry Breaking and Turbulence in Perturbed Plane Couette Flow

ME 321: FLUID MECHANICS-I

4. BACKWATER EFFECTS OF PIERS IN SUBCRITICAL FLOW 5. Report Date October Performing Organization Code

DIMENSIONS AND UNITS

(z + n) 2. n=0. 2 (z + 2) (z + n). 2 We d like to compute this as an integral. To this end, we d like a function with residues

UNIFORM FLOW CRITICAL FLOW GRADUALLY VARIED FLOW

EXAMPLE SHEET FOR TOPIC 3 AUTUMN 2013

Shell Balances in Fluid Mechanics

Transcription:

CHPTER Problem : (a) Trapeoidal channel with side slopes m and m ( b + m + m ) T b + ( m ) + m + P b + + m + m D / T R / P (b) Trapeoidal channel with one vertical side Set m and m m in the equations given in part (a). (c) Right triangular channel Set m, b, and m m in the equations given in part (a). Problem : (a) From the problem statement: γ 6.4 lbf/ft Y c depth to centroid ft d ( ft/ft) 4 ft ( ft/ft) 4 ft /ft B using Equation.9 Fp γ Yc 6.4()(4) 499 lbf / foot The e hdrostatic pressure force is normal to the vertical sidewall. (b) From the problem statement: γ 6.4 lbf/ft Y c depth to centroid ft (d +(md) ) / ( ft/ft) (4 +(x4) ) / ft ( ft/ft) 8.94 ft /ft B using Equation.9 Fp γ Yc 6.4()(4) 6 lbf / foot The hdrostatic pressure force is normal to the inclined side. Problem :

v.5v s * Let s /. Then v.5v * Define q discharge per unit width. B definition (see Equation.) q vd.5v * d [.5v ] d [ v ] d *.5 * q.5v*.5v*.5v* ( ) Problem 4: [ ] [ ] Noting that q discharge per unit width and s / as in Problem, b definition (see Equation.) ( ) q.5v *.5v * Because >>, we have (-). Therefore.5v* Problem 5: For the velocit distribution given, obviousl, the velocit is imum at the free surface. Substituting in v.5v* s we obtain v.5v*.5v s with s /. * 4

Problem 6: Using the results of Problems 4 and 5.5v* v.5v * with s /. Problem 7: We found an expression for in Problem 4. Here we will determine the value of for which v. In other words with s /.5v*.5v * and. 7.78 / (.78).78 The point velocit at distance.7 from the bottom or.6 from the free surface will be equal to the cross sectional average velocit. Therefore, the velocit measured at.6 from the surface will be a good approximation to the average velocit. Problem 8: With s /, we have v.5v * B definition β v d Using the velocit distribution given, for unit width, we can write (.5v *) β d ( ) 5

Let us first evaluate the integration d ( )( ) d ( d + [ ] d d + [ ( ) ( ) ] d + d ) d d ( ) + ( ) ( ) (*) lso from Problem 4.5v* (.5v* ) (.5v*) + With >> and (-) ( ) (.5v* ) + (**) Substituting Equations (*) and (**) into the expression for β β [(.5v ) ] * ( ) + ( ) ( ) (.5v* ) + Noting (-) and simplifing + + ( ) ( ) β + From Problem 6 + 6

v Substituting this into the expression for β and rearranging β v + Problem 9: / / τ.7 v *.6m / s ρ From Problem 4 (.94).5v.5v (.5)(.6) s (.) s q (.94)(.4).m / s * * From Problem 5 v. (.94) (.) v β + s + (.)..4m / s g m m gm Rate of momentum transfer βρ q (.)( )(. )(.4 ) 894 / m m s s s v α + v + (.) (.). ρ g m m Nm Rate of inetic transfer α q (.) ( )(. )(.4 ) 6 / m m s s s Problem : m x m m 4 m x 4 m 6 m.5( m x m) m 7

Q + +.5() +.5(6) +.() 7. m / s Q Q 7..79 m / s + + + 6 + Problem : From Equation.5 + +.5 () +.5 (6) +. β.79 (47) Then b using Equation. with ρ g/m ().4 Rate of momentum transfer βρ Q.4()(7.)(.79) 4,8 g m / s Liewise, from Equation. α + +.5 () +.5 (6) +. ().79 (47).45 Then b using Equation.9 ρ Rate of inetic energ transfer α Q Problem :.45 (7.)(.79) 8,57 g m / s Q Q. fps ( b + m).5(5 +.5) 5.6 8 ( b + m).5(5 +.5) 5.6 R. 86 P b + + m 5 + (.5) + 9. ( b + m).5(5 +.5) 5.6 D. ft b + m 5 +.5 7.6 ft (a) Using Equation. 4R 4R 4(.8)(.86) R e 5 ν ν.7 The flow is turbulent.,95, (b) Using Equation.4 F r gd.8...5 8

The flow is subcritical. Problem : (a) Nonuniform (b) Nonuniform (c) Uniform (d) Nonuniform Problem 4: (a) Unstead (b) Stead (c) Stead Problem 5: erif that ( Y C ) Consider a horiontal strip of flow area having a length of b and thicness of d and extending from one side of a flow section to the other side. Suppose the vertical distance between the centroid of this strip and the channel bottom is. Then b definition ( Y C ) ( ) bd Using the Leibnit rule, we can write this as ( Y C ) ( ) bd + ( ) bd ( ) bd The last two terms on the right hand side are ero. Then ( Y ) C ( ) bd ( bd) ( bd) x x Since and b are not functions of x at a given section, the last term on the right hand side is ero. lso, since is not a function of and b and d are not functions of x ( Y C ) ( bd) bd x 9