MAHALAKSHMI ENGINEERING COLLEGE TIRUCHIRAPALLI

Similar documents
CE MECHANICS OF FLUIDS UNIT I


HYDRAULICS STAFF SELECTION COMMISSION CIVIL ENGINEERING STUDY MATERIAL HYDRAULICS

Fluid Mechanics Introduction

Fluids and their Properties

Homework of chapter (1) (Solution)

Fluid Mechanics-61341

Petroleum Engineering Dept. Fluid Mechanics Second Stage Dr. Ahmed K. Alshara

Introduction to Marine Hydrodynamics

University of Hail Faculty of Engineering DEPARTMENT OF MECHANICAL ENGINEERING. ME Fluid Mechanics Lecture notes. Chapter 1

1. The Properties of Fluids

VALLIAMMAI ENGINEERING COLLEGE SRM Nagar, Kattankulathur

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

R09. d water surface. Prove that the depth of pressure is equal to p +.

INSTITUTE OF AERONAUTICAL ENGINEERING Dundigal, Hyderabad AERONAUTICAL ENGINEERING QUESTION BANK : AERONAUTICAL ENGINEERING.

MM303 FLUID MECHANICS I PROBLEM SET 1 (CHAPTER 2) FALL v=by 2 =-6 (1/2) 2 = -3/2 m/s

Petroleum Engineering Department Fluid Mechanics Second Stage Assist Prof. Dr. Ahmed K. Alshara

1 FLUIDS AND THEIR PROPERTIES

CHAPTER 1 Fluids and their Properties

MECHANICAL PROPERTIES OF FLUIDS:

FRIDAYS 14:00 to 15:40. FRIDAYS 16:10 to 17:50

1. Introduction, fluid properties (1.1, 2.8, 4.1, and handouts)

df da df = force on one side of da due to pressure

Theory of turbomachinery. Chapter 1

CE FLUID MECHANICS AND MECHINERY UNIT I

Middle East Technical University Department of Mechanical Engineering ME 305 Fluid Mechanics I Fall 2018 Section 4 (Dr.

PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [ ] Introduction, Fundamentals of Statics

REE Internal Fluid Flow Sheet 2 - Solution Fundamentals of Fluid Mechanics

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

Chapter 1 Fundamentals

ENGR 292 Fluids and Thermodynamics

CE MECHANICS OF FLUIDS

Fluid Mechanics Abdusselam Altunkaynak

P = 1 3 (σ xx + σ yy + σ zz ) = F A. It is created by the bombardment of the surface by molecules of fluid.

INTRODUCTION DEFINITION OF FLUID. U p F FLUID IS A SUBSTANCE THAT CAN NOT SUPPORT SHEAR FORCES OF ANY MAGNITUDE WITHOUT CONTINUOUS DEFORMATION

ME 262 BASIC FLUID MECHANICS Assistant Professor Neslihan Semerci Lecture 4. (Buoyancy and Viscosity of water)

Fluid Mechanics II Viscosity and shear stresses

CHARACTERISTIC OF FLUIDS. A fluid is defined as a substance that deforms continuously when acted on by a shearing stress at any magnitude.

ACE Engineering College

Chapter 1 INTRODUCTION

UNIT I FLUID PROPERTIES AND STATICS

Chapter 1 Fluid Proper2es. CE Fluid Mechanics Diogo Bolster

CHAPTER (2) FLUID PROPERTIES SUMMARY DR. MUNZER EBAID MECH.ENG.DEPT.

Lecturer, Department t of Mechanical Engineering, SVMIT, Bharuch

A drop forms when liquid is forced out of a small tube. The shape of the drop is determined by a balance of pressure, gravity, and surface tension

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

Chapter 4 DYNAMICS OF FLUID FLOW

Chapter 1 Fluid Characteristics

FE FORMULATIONS FOR PLASTICITY

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


Pressure variation with direction. Pressure variation with location How can we calculate the total force on a submerged surface?

Dynamic (absolute) Viscosity

UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation.

BFC FLUID MECHANICS BFC NOOR ALIZA AHMAD

Chapter 10 - Mechanical Properties of Fluids. The blood pressure in humans is greater at the feet than at the brain

Downloaded from Downloaded from / 1

Phase transition. Asaf Pe er Background

Non-Newtonian fluids is the fluids in which shear stress is not directly proportional to deformation rate, such as toothpaste,

Polymerization Technology Laboratory Course

BME-A PREVIOUS YEAR QUESTIONS

PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK

LECTURE 1 THE CONTENTS OF THIS LECTURE ARE AS FOLLOWS:

ch-01.qxd 8/4/04 2:33 PM Page 1 Part 1 Basic Principles of Open Channel Flows

COURSE NUMBER: ME 321 Fluid Mechanics I. Fluid: Concept and Properties

Liquids and solids are essentially incompressible substances and the variation of their density with pressure is usually negligible.

STRESS, STRAIN AND DEFORMATION OF SOLIDS

SECOND ENGINEER REG. III/2 APPLIED MECHANICS

STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS

Sliding Contact Bearings

DIVIDED SYLLABUS ( ) - CLASS XI PHYSICS (CODE 042) COURSE STRUCTURE APRIL

PHYSICS. Course Structure. Unit Topics Marks. Physical World and Measurement. 1 Physical World. 2 Units and Measurements.

CH.1 Overview of Fluid Mechanics/22 MARKS. 1.1 Fluid Fundamentals.

1 atm = 1.01x10 Pa = 760 Torr = 14.7 lb / in

We may have a general idea that a solid is hard and a fluid is soft. This is not satisfactory from

COVENANT UNIVERSITY NIGERIA TUTORIAL KIT OMEGA SEMESTER PROGRAMME: MECHANICAL ENGINEERING

On Gravity Waves on the Surface of Tangential Discontinuity

MECHANICAL PROPERTIES OF FLUIDS

Chapter 13 ELASTIC PROPERTIES OF MATERIALS

What s important: viscosity Poiseuille's law Stokes' law Demo: dissipation in flow through a tube

Agricultural Science 1B Principles & Processes in Agriculture. Mike Wheatland

A Model Answer for. Problem Set #4 FLUID DYNAMICS

Equilibrium. the linear momentum,, of the center of mass is constant

Diffuse Interface Models for Metal Foams

Fluid Mechanics 3502 Day 1, Spring 2018

Day 3. Fluid Statics. - pressure - forces

QUESTION BANK DEPARTMENT: CIVIL SEMESTER: III SUBJECT CODE: CE2201 SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A

u y

a) Derive general expressions for the stream function Ψ and the velocity potential function φ for the combined flow. [12 Marks]

1 Lecture 5. Linear Momentum and Collisions Elastic Properties of Solids

Laboratory 9: The Viscosity of Liquids

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

Fluid Properties and Units

Assignment Set 2 - Solutions Due: Wednesday October 6; 1:00 pm

Universal Viscosity Curve Theory

SOLID AND FLUID MECHANICS (Two Mark Question and Answers)

UNIT II CONVECTION HEAT TRANSFER

Part II Fundamentals of Fluid Mechanics By Munson, Young, and Okiishi

Fluid Mechanics Testbank By David Admiraal

Efficiencies. Damian Vogt Course MJ2429. Nomenclature. Symbol Denotation Unit c Flow speed m/s c p. pressure c v. Specific heat at constant J/kgK

Transcription:

MAHALAKSHMI ENGINEERING COLLEGE TIRUCHIRAPALLI 6113 DEPARTMENT: CIVIL SUB.CODE/ NAME: CE6303/ MECHANICS OF FLUIDS SEMESTER: III UNIT-1 FLUID PROPERTIES TWO MARK QUESTIONS AND ANSWERS 1. Define fluid mechanics.(auc May/June 010) It is the branch of science, which deals with the behavior of the fluids (liquids or gases) at rest as well as in motion.. Define Mass Density..(AUC Nov/Dec 010) Mass Density or Density is defined as ratio of mass of the fluid to its volume (V) Density of water = 1 gm/cm 3 or 1000 kg / m 3. 3. Define Secific Weight..(AUC May/June 010) It is the ratio between weight of a fluid to its volume. Weight of fluid Mass of fluid w g g Volume of fluid w g Unit: N / m 3 Volume of fluid 4. Define Viscosity. (AUC Nov/Dec 009) Viscosity is defined as the roerty of fluid, which offers resistance to the movement of one layer of fluid over another adjacent layer of fluid. PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 1

When two layers move one over the other at different velocities, say u and u+, the viscosity together with relative velocity causes a shear stress acting between the fluid layers. The to layer causes a shear stress on the adjacent lower layer while the lower layer causes a shear stress on the adjacent to layer. This shear stress is roortional to the rate of change of velocity. Coefficient of namic viscosity (or) only viscosity / = rate of shear strain 5. Define Secific Volume. (AUC May/June 011) Volume er unit mass of a fluid is called secific volume Unit: m 3 / kg. 6. Define Secific Gravity. (AUC May/June 013) Secific gravity is the ratio of the weight density or density of a fluid to the weight density or density of standard fluid. It is also called as relative density. Unit : Dimension less. Denoted as: S S (forliquid) Weight density of liquid Weight density of water S (for gases)= 7. Calculate the secific weight, density and secific gravity of 1 litre of liquid which weighs 7 N. (AUC May/June 013) Solution: Given V 1ltre 1 1000 m 3 PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page

W = 7 N i. S. Weight (w) weight 7 N volume 1 m 3 1000 7000 N / m 3 ii Density () w 7000 N kg / m 3 9.81 m 3 713..5 Kg / m 3 g iii. S. Gravity (S) Density of liquid 713.5 Density of water 1000 (Density of water = 1000 kg / m 3) S = 0.7135 8. State Newton s Law of Viscosity. (AUC Nov/Dec 013) It states that the shear stress ( ) on a fluid element layer is directly roortional to the rate of shear strain. The constant of roortionality is called the co-efficient of viscosity 9. Name the Tyes of fluids. (AUC Nov/Dec 01) 1. Ideal fluid. Real fluid 3. Newtonian fluid 4. Non-Newtonian fluid. 5. Ideal lastic fluid 10. Define Kinematic Viscosity. (AUC Nov/Dec 011) It is defined as the ratio between the namic viscosity and density of fluid. PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 3

1 Stoke Cm 1 m 10 4 m / s. S 100 S Centistoke means 1 stoke 100 11. Determine the secific gravity of a fluid having viscosity 0.05 oise and Kinematic viscosity 0.035 stokes. Given: Viscosity, μ = 0.05 oise = (0.05 / 10) Ns / m. Kinematic viscosity ν = 0.035 stokes = 0.035 cm / s = 0.035 x 10-4 m / s 0.035 10 4 0.05 1 10 148.5kg / m 3 Density of liquid 148.5 1. Define Comressibility. Comressibility is the recirocal of the bulk molus of elasticity, K which is defined as the ratio of comressive stress to volumetric strain. 13. Define Surface Tension. Surface tension is defined as the tensile force acting on the surface of a liquid in contact with a gas or on the surface between two immiscible liquids such that the contact surface behaves like a membrance under tension. Unit: N / m. PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 4

14. Define Caillarity: Caillary is defined as a henomenon of rise of a liquid surface is a small tube relative to adjacent general level of liquid when the tube is held vertically in the liquid. The resistance of liquid surface is known as caillary rise while the fall of the liquid surface is known as caillary deression. It is exressed in terms of cm or mm of liquid. 15. The Caillary rise in the glass tube is not to exceed 0. mm of water. Determine its minimum size, given that surface tension of water in contact with air = 0.075 N/m Solution: Caillary rise, h = 0. mm = 0. x 10 3 m Surface tension 0.075N/m Let, Diameter of tube = d Angel for water = 0 Density for water = 1000 kg / m h 4 g d 0. 10 4 0.075 3 1000 9.81 d d 4 0.075 1000 9.81 0. 10 3 Minimum of the tube = 14.8 cm. 0.148m 14.8cm 16. Find out the minimum size of glass tube that can be used to measure water levelif the caillary rise in the tube is to be restricted to mm. Consider surface tension of water in contact with air as 0.073575 N/m. Solution: Caillary rise h =.0 mm =.0 10 3 m PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 5

Let, diameter = d Density of water = 1000 kg / m 3 0. 073575 N / m Angle for water 0 \ PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 6

h 4.0 10 3 4 0.073575 g d 1000 9.81 d d = 0.015 m = 1.5 cm. Thus the minimum diameter of the tube should be 1.5 cm. 17. Define Real fluid and Ideal fluid. Real Fluid: A fluid, which ossesses viscosity, is known as real fluid. All fluids, in actual ractice, are real fluids. Ideal Fluid: A fluid, which is incomressible and is having no viscosity, is known as an ideal fluid. Ideal fluid is only an imaginary fluid as all the fluids, which exist, have some viscosity. 18. Write down the exression for caillary fall. PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 7

19. Two horizontal lates are laced 1.5 cm aart. The sace between them being filled with oil of viscosity 14 oises. Calculate the shear stress in oil if uer late is moved with a velocity of.5 m/s. Solution: Given: Distance between the lates, = 1.5 cm = 0.015m. Viscosity μ = 14 oise = 14 / 10 Ns / m Velocity of uer late, u =.5 m/sec. Shear stress is given by equation as τ = μ ( / ). Where = change of velocity between the lates = u 0 = u =.5 m/sec. = 0.015m. τ = (14 /10) X (.5 / 0.015) = 80 N/m. PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 8

PART B 1.Calculate the caillary effect in millimeters a glass tube of 4mm diameter, whenimmersed in (a) water (b) mercury. The temerature of the liquid is 0 0 C and the values of the surface tension of water and mercury at 0 0 C in contact with air are 0.073575 and 0.51 N/m resectively. The angle of contact for water is zero that for mercury 130 0. Take secific weight of water as 9790 N / m 3 (AUC May/June 009) (AUC May/June 011) Given: Diameter of tube d = 4 mm = 4 10 3 m Caillary effect (rise or deression) h 4 cos g d Surface tension in kg f/m Angle of contact and = density i. Caillary effect for water 0.073575 N / m, 0 0 998 kg / m 3 @ 0 0 c 4 0.73575 Cos0 0 h 998 9.81 4 10 3 = 7.51 mm. 7.51 10 3 m Caillary effect for mercury : 0.51 N / m, 130 0 s gr 1000 13.6 1000 13600kg /m 3 PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 9

.46 10 3 m = -.46 mm. -Ve indicates caillary deression.. A cylinder of 0.6 m 3 in volume contains air at 50 0 C and 0.3 N/ mm absoluteressure. The air is comressed to 0.3 m 3. Find (i) ressure inside the cylinder assuming isothermal rocess (ii) ressure and temerature assuming adiabatic rocess. Take K = 1.4 (AUC May/June 010) Given: Initial volume 1 0.36m 3 Pressure P 1 = 0.3 N/mm 0.3 10 6 N / m Temerature, t 1 = 50 0 C T 1 = 73 + 50 = 33 0 K Final volume, 0.3m 3 K = 1.4 i. Isothermal Process: P Cons tan t (or ) Cons tan t 1 A A A 1 1 30 10 4 0.6 0.3 0.6 10 6 N / m = 0.6 N / mm PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 10

ii) adiabatic rocess K Cons tan t or K cons tan t. K 1 1 K K 0.6 1.4 1 1 K 30 10 4 30 10 4 1.4 0.3 0.791 10 6 N / m 0.791N / mm For temerature, RT, k cons tan t RT and RT k cons tan t RT k 1 Cons tan t T k 1 Cons tan t R is also cons tan t T V k 1 T V k 1 1 1 V 1 k 1 T T 33 1 V 0.6 1.4 1.0 0.3 33 0.4 46. 0 K t 46. 73 153. 0 C PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 11

3. If the velocity rofile of a fluid over a late is a arabolic with the vertex 0 cmfrom the late, where the velocity is 10 cm/sec. Calculate the velocity gradients and shear stress at a distance of 0,10 and 0 cm from the late, if the viscosity of the fluid is 8.5 oise. (AUC May/June 010) Given, conditions. Distance of vertex from late = 0 cm. Velocity at vertex, u = 10 cm / sec. Viscosity, 8.5 oise 8.5 Ns 10 m 0.85 Parabolic velocity rofile equation, u ay by C -------------- (1) Where, a, b and c constants. Their values are determined from boundary i) At y = 0, u = 0 ii) At y = 0cm, u = 10 cm/se. iii) At y = 0 cm, 0 Substituting (i) in equation (1), C = 0 Substituting (ii) in equation (1), 10 a 0 b 400 a 0b -----------() Substituting (iii) in equation (1), ay b solving 1 and, we get, 400 a 0 b 0 ( ) 40 a + b = 0 800 a 0 b 0 b = - 40 a 10 400 a 0 b 40 a 400 a 800 a 400 a 0 a 0 b 40a b-----------(3) a 10 3 400 10 0.3 PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 1

b 40 0.3 1. Substituting a, b and c in equation (i) u 0.3y 1y 0.3 y 1 0.6 y 1 Velocity gradient at y = 0, Velocity gradient, at y =10 cm, Velocity gradient, y 0 y 10 0.6 0 1 1 / s. 0.6 10 1 6 1 6 / s. at y = 0 cm, Velocity gradient, 0.6 0 1 1 1 0 Shear Stresses: Shear stresses is given by, i. Shear stress at y = 0, ii. Shear stress at y = 10, iii.shear stress at y = 0, y 0 y 0 y 10 y 0 0.85 1.0 10.N / m 0.85 6.0 5.1N / m 0.85 0 0 PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 13

4. A 15 cm diameter vertical cylinder rotates concentrically inside another cylinderof diameter 15.10 cm. Both cylinders are 5 cm high. The sace between the cylinders is filled with a liquid whose viscosity is unknown. If a torque of 1.0 Nm is required to rotate the inner cylinder at 100 rm determine the viscosity of the fluid. (AUC Nov/Dec 011) Solution: Diameter of cylinder = 15 cm = 0.15 m Diameter of outer cylinder = 15.10 cm = 0.151 m Length of cylinder L = 5 cm = 0.5 m Torque T= 1 Nm ; N = 100 rm. Viscosity = Tangential velocity of cylinder u DN 0.15 100 60 60 0.7854 m / s Surface area of cylinder A D L 0.15 0.5 = 0.1178 m u 0 u 0.7854 m / s 0.151 0.150 0.0005 m 0.7854 0.0005 Shear force, F Shear Stress Area 0.7854 0.0005 0.1178 Torque T F D 1.0 0.7854 0.15 0.1178 0.0005 1.0 0.0005 0.7854 0.1178 0.15 0.864 Ns / m PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 14

0.864 10 8.64 oise. 5. The namic viscosity of oil, used for lubrication between a shaft and sleeve is 6 oise. The shaft is of diameter 0.4 m and rotates at 190 rm. Calculate the ower lost in the bearing for a sleeve length of 90 mm. The thickness of the oil film is 1.5mm. (AUC Nov/Dec 013) Given, 6 oise D = 0.4 m N = 190 rm. 6 Ns 0.6 Ns 10 m m L 90 mm 90 10 3 m t 1.5 mm 1.5 10 3 m Power NT W 60 T force D Nm. F Shear stress Area DL N / m u DN m / s. 60 Tangential Velocity of shaft, u DN 0.4 190 60 60 3.98 m / s. = change of velocity = u 0 = u = 3.98 m/s. t 1.5 10 3 m. 3.98 10 1.5 10 3 159N / m Shear force on the shaft F = Shear stress x Area PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 15

F 159 D L 159 0.4 90 10 3 180.05N Torque on the shaft, T Force D 0.4 180.05 36.01 Ns. Power lost NT 190 36.01 60 60 716.48W 6.If the velocity distribution over a late is given byu y y in which U is the 3 velocity in m/s at a distance y meter above the late, determine the shear stress at y = 0 and y = 0.15 m. Take namic viscosity of fluid as 8.63 oise. (AUC May/June 013) Given: u y y 3 3 y 0 y 0 y 0.15 3 3 3 0.17 0.667 0.30 8.63 oise 8.63 SI units = 0.863 Ns / m 10 PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 16

i. Shear stress at y = 0 is given by 0 y 0 0.863 0.667 0.5756 N / m ii. Shear stress at y = 0.15 m is given by y 0.15 y 0.15 0.863 0.367 0.3167 N / m 7.The diameters of a small iston and a large iston of a hydraulic jack at3cm and10 cm resectively. A force of 80 N is alied on the small iston Find the load lifted by the large iston when: a. The istons are at the same level b. Small iston in 40 cm above the large iston. The density of the liquid in the jack in given as 1000 kg/m 3 (AUC Nov/Dec 01) Given: Dia of small iston d = 3 cm. Area of small iston, a d 4 4 3 7.068cm Dia of large iston, D = 10 cm P Area of larger iston, A 4 10 78.54cm Force on small iston, F = 80 N Let the load lifted = W a. When the istons are at the same level Pressure intensity on small iston P F 80 N / cm a 7.068 PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 17

This is transmitted equally on the large iston. Pressure intensity on the large iston 80 7.068 Force on the large iston = Pressure x area = 80 7.068 x 78.54 N = 888.96 N. b. when the small iston is 40 cm above the large iston Pressure intensity on the small iston F 80 N / cm a 7.068 Pressure intensity of section A A F ressure intensity e of height of 40 cm of liquid. P = gh. a But ressure intensity e to 40cm. of liquid g h 1000 9.81 0.4N / m 1000 9.81 0.4 N/cm 0.394N/cm 10 4 Pressure intensity at section 80 A A 0.394 7.068 = 11.3 + 0.394 = 11.71 N/cm Pressure intensity transmitted to the large iston = 11.71 N/cm Force on the large iston = Pressure x Area of the large iston 11.71 A 11.71 78.54 = 919. 7 N PREPARED BY K.M.SHAMEER (CE6303-MECHANICS OF FLUID) Page 18