Useful concepts associated with the Bernoulli equation. Dynamic

Similar documents
2.The lines that are tangent to the velocity vectors throughout the flow field are called steady flow lines. True or False A. True B.

FLUID MECHANICS. Chapter 3 Elementary Fluid Dynamics - The Bernoulli Equation

Chapter 3 Bernoulli Equation

The Bernoulli Equation

3.25 Pressure form of Bernoulli Equation

Objectives. Conservation of mass principle: Mass Equation The Bernoulli equation Conservation of energy principle: Energy equation

Rate of Flow Quantity of fluid passing through any section (area) per unit time

CEE 3310 Control Volume Analysis, Oct. 7, D Steady State Head Form of the Energy Equation P. P 2g + z h f + h p h s.

CEE 3310 Control Volume Analysis, Oct. 10, = dt. sys

Chapter Four fluid flow mass, energy, Bernoulli and momentum

Mass of fluid leaving per unit time

(British) (SI) British Metric L T [V] = L T. [a] = 2 [F] = F = 2 T

CHAPTER 3 BASIC EQUATIONS IN FLUID MECHANICS NOOR ALIZA AHMAD

An-Najah National University Civil Engineering Departemnt. Fluid Mechanics. Chapter [2] Fluid Statics

Chapter 5 Mass, Momentum, and Energy Equations

Fluid Mechanics-61341

FE Fluids Review March 23, 2012 Steve Burian (Civil & Environmental Engineering)

Chapter (6) Energy Equation and Its Applications

FLUID MECHANICS PROF. DR. METİN GÜNER COMPILER

Chapter 5: Mass, Bernoulli, and Energy Equations

AER210 VECTOR CALCULUS and FLUID MECHANICS. Quiz 4 Duration: 70 minutes

Basic Fluid Mechanics

Measurement of cyclone separator

Fluid Dynamics. Type of Flows Continuity Equation Bernoulli Equation Steady Flow Energy Equation Applications of Bernoulli Equation

Chapter 7 Energy Principle

For example an empty bucket weighs 2.0kg. After 7 seconds of collecting water the bucket weighs 8.0kg, then:

EGN 3353C Fluid Mechanics

BERNOULLI EQUATION. The motion of a fluid is usually extremely complex.

5 ENERGY EQUATION OF FLUID MOTION

HOMEWORK ASSIGNMENT ON BERNOULLI S EQUATION

If a stream of uniform velocity flows into a blunt body, the stream lines take a pattern similar to this: Streamlines around a blunt body

3.8 The First Law of Thermodynamics and the Energy Equation

f= flow rate (m 3 /s) A = cross-sectional area of the pipe (m 2 ) v= flow speed (m/s)

MASS, MOMENTUM, AND ENERGY EQUATIONS

Theory of turbomachinery. Chapter 1

New Website: Mr. Peterson s Address:

BERNOULLI EQUATION. The motion of a fluid is usually extremely complex.

Stream Tube. When density do not depend explicitly on time then from continuity equation, we have V 2 V 1. δa 2. δa 1 PH6L24 1

Chapter 4 DYNAMICS OF FLUID FLOW

vector H. If O is the point about which moments are desired, the angular moment about O is given:

주요명칭 수직날개. Vertical Wing. Flap. Rudder. Elevator 수평날개

Basics of fluid flow. Types of flow. Fluid Ideal/Real Compressible/Incompressible

6.1 Momentum Equation for Frictionless Flow: Euler s Equation The equations of motion for frictionless flow, called Euler s

Consider a control volume in the form of a straight section of a streamtube ABCD.

1.060 Engineering Mechanics II Spring Problem Set 4

A Model Answer for. Problem Set #4 FLUID DYNAMICS

Chapter 7 The Energy Equation

ME 3560 Fluid Mechanics

PART II. Fluid Mechanics Pressure. Fluid Mechanics Pressure. Fluid Mechanics Specific Gravity. Some applications of fluid mechanics

Fluid Mechanics. du dy

Unit C-1: List of Subjects

ME 316: Thermofluids Laboratory

10.52 Mechanics of Fluids Spring 2006 Problem Set 3

Dimensions represent classes of units we use to describe a physical quantity. Most fluid problems involve four primary dimensions

Study fluid dynamics. Understanding Bernoulli s Equation.

MAE 101A. Homework 3 Solutions 2/5/2018

In steady flow the velocity of the fluid particles at any point is constant as time passes.

ME3560 Tentative Schedule Spring 2019

AE301 Aerodynamics I UNIT A: Fundamental Concepts

CLASS SCHEDULE 2013 FALL

ME3560 Tentative Schedule Fall 2018

Q1 Give answers to all of the following questions (5 marks each):

Chapter 5 Mass, Bernoulli, and Energy Equations Chapter 5 MASS, BERNOULLI, AND ENERGY EQUATIONS

Physics Courseware Physics I

Lesson 6 Review of fundamentals: Fluid flow

5. The Bernoulli Equation

Introduction to Turbomachinery

Control Volume Revisited

1 st Law Analysis of Control Volume (open system) Chapter 6

Part A: 1 pts each, 10 pts total, no partial credit.

AE301 Aerodynamics I UNIT A: Fundamental Concepts

Fluids. Fluids in Motion or Fluid Dynamics

Chapter 10: Flow Flow in in Conduits Conduits Dr Ali Jawarneh

Physics 123 Unit #1 Review

Chapter 5: Mass, Bernoulli, and

Approximate physical properties of selected fluids All properties are given at pressure kn/m 2 and temperature 15 C.

Hydromechanics: Course Summary

Pressure in a fluid P P P P

SYSTEMS VS. CONTROL VOLUMES. Control volume CV (open system): Arbitrary geometric space, surrounded by control surfaces (CS)

Chapter 1 Fundamentals

2 Internal Fluid Flow

Lecture Note for Open Channel Hydraulics

Pressure in stationary and moving fluid Lab- Lab On- On Chip: Lecture 2

New Website: M P E il Add. Mr. Peterson s Address:

FLOW MEASUREMENT IN PIPES EXPERIMENT

ENGINEERING FLUID MECHANICS. CHAPTER 1 Properties of Fluids

Lecture 3 The energy equation

Chapter 5. Mass and Energy Analysis of Control Volumes

!! +! 2!! +!"!! =!! +! 2!! +!"!! +!!"!"!"

Thermodynamics ENGR360-MEP112 LECTURE 7

Hydraulics and hydrology

Chapter 11. Fluids. continued

University of Engineering and Technology, Taxila. Department of Civil Engineering

equation 4.1 INTRODUCTION

Signature: (Note that unsigned exams will be given a score of zero.)

TOPICS. Density. Pressure. Variation of Pressure with Depth. Pressure Measurements. Buoyant Forces-Archimedes Principle

V/ t = 0 p/ t = 0 ρ/ t = 0. V/ s = 0 p/ s = 0 ρ/ s = 0

Angular momentum equation

STATIC, STAGNATION, AND DYNAMIC PRESSURES

57:020 Mechanics of Fluids and Transfer Processes CONSERVATION OF MASS, LINEAR MOMENTUM, AND ENERGY IN A SLUICE GATE FLOW. dt dt. d ( momentum.

Transcription:

Useful concets associated with the Bernoulli equation - Static, Stagnation, and Dynamic Pressures Bernoulli eq. along a streamline + ρ v + γ z = constant (Unit of Pressure Static (Thermodynamic Dynamic Hydrostatic Piezometer tube Physical meaning of each term Velocity of stream i st term (Static ressure, : Only due to the fluid weight = 3 + γ h3 = γ h4 3 + γh3 = γh where 3 = γ h4 3 (h 4-3 : Piezometer reading ii nd term (Dynamic ressure, ρ v : Pressure increase or decrease due to fluid motion iii 3 rd term (Gravitational otential, γ z : Pressure change due to elevation change Between Point ( and Point ( on the same streamline, ρ v = + ρv + γz = constant because z = z (No elevation change v = 0 (Stagnated by a tube inserted +

Difference in between iezometer and tube inserted into a flow = γh (Stagnation ressure ρv = = γh γh (Elevation change, H h: Due to dynamic ressure Point (: Stagnation oint ( V = 0 Line through oint (: Stagnation streamline iv Total ressure T = + ρ V + γz = constant (Along a streamline Secial alication of Static and Stagnation Pressure - Determination of fluid seed (Pitot-static tube By measuring ressure at oints (3 and (4 and neglecting the elevation effect (e.g. gases At oint (3, 3 = + ρ V (Stagnation Pressure where and V: Static ressure and fluid velocity at ( At onit (4 (Small holes, 4 = = (Static ressure ~ Piezometer Then, 3 ( 4 = ρ V 3 4 V ρ = : Pitot-static tube

Here Here Photo-detector Wheel How to detect the wheel seed (e.g. Car and Comuter mouse etc.

How to use the Bernoulli equation (Examles Choose oints ( and ( along a streamline = + ρv + γz : 6 variables (,, V, V, z, z 5 more conditions from the roblem descrition E.g. Free Jets (A jet of liquid from large reservoir Question: Find V of jet stream from a nozzle of container Consider a situation shown Ste. Select one streamline between ( & ( Ste. Aly the Bernoulli eq. between ( & ( = + ρv + γz because = 0: Gauge ressure (The atmoshere V = 0 (Large container Negligible change of fluid level = 0 (Why? [ = 4 (Normal Bernoulli eq.] Then, γ h = ρ V (If we choose z as h and z as 0 or γh V = = gh : Velocity at the exit lane of nozzle ρ

Velocity at any oint [e.g. (5 in the figure] outside the nozzle, v = g( h + H (H: Distance from the nozzle : Conversion of P. E. to K.E. without viscosity (friction cf. Free body falling from rest without air resistance. In case of horizontal nozzle shown, v < < (Elevation difference v v3 By assuming d << h, v : Average velocity at the nozzle E.g. Confined Flows - Fluid flowing within a container connected with nozzles and ies What to know - We can t use the atmosheric as a standard - But, we have one more useful concet of conservation of mass : No change of fluid mass in fixed volume (continuity equation Mass flow rate, m& (kg/s or slug/s for a steady flow Mass of fluid entering the container across inlet er unit time = Mass of fluid leaving the container across outlet er unit time,

δm V ta m ρ δ ρ & = = (Inlet VδtA δm = = = m& (Outlet δt δt δt δt Or δm m& = δ t (kg/s = ρ Q (Q: Volume flowrate, m 3 /s For a time interval δ t, m & = = ρ Q = ρav = ρ AV = ρq m For a incomressible fluid, ρ = ρ V AV A = or Q = Q & Change in area Change in fluid velocity ( A V = AV Change in ressure ( = + ρv + γz Increase in velocity Decrease in ressure : Blow off the roof by hurricane, Cavitation damage, etc.

E.g. 3 Flowrate Measurement Case : Determine Q in ies and conduits (Closed container Consider three tyical devices (Deend on the tye of restriction Ste. At section ( : Low V, High At section ( : High V, Low Ste. Aly the Bernoulli Eq. For a horizontal flow (z = z = + ρv V ( = ρ [ ( V / V ] Ste 3. Use the continuity Eq. Q = AV = AV = A ( ρ[ ( A / A ] where A & A : Known : Measured by gages

Case : Determine Q in flumes and irrigation ditches (Oen channer Tyical devices: Sluice gate (Oen bottom & Shar-crested weir (Oen to Consider a sluice gate shown Bernoulli Eq. & Continuity Eq. [( (] = + ρv + γz g( z z V = ( V / V ( = = 0 and Q = A V = bz V = A V = bz V Finally, the flowrate, Q = bz g( z ( z z / z In case of z >> z or z z z or z / z << Q = bz gz or V gz The shar-crested weir (Oen to (If similar to horizontal free stream Then, Average velocity across the to of the weir Flow area for the weir Hb gh Q = C Hb gh = C b H 3/ g

Energy Line (EL and the Hydraulic Grade Line (HGL - Geometrical Interretation of the Bernoulli Eq. Bernoulli eq.: Conserved total energy along streamline, i.e. V + + z = constant on a streamline = H (Unit of Length γ g Heads: : Pressure head, γ H: Total head v : Velocity head, z: Elevation head g Energy line (EL: Reresentation of Energy versus Heads ( (: Elevation head Pressure head Velocity head ( ( (3 ( (3: Elevation head Pressure head Velocity head e.g. Flow from tank