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

Similar documents
Homework of chapter (1) (Solution)

Fluids and their Properties

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

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

The online of midterm-tests of Fluid Mechanics 1

Figure 3: Problem 7. (a) 0.9 m (b) 1.8 m (c) 2.7 m (d) 3.6 m

CE MECHANICS OF FLUIDS UNIT I

Introduction to Marine Hydrodynamics

CHAPTER 1 Fluids and their Properties

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

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

Fluid Mechanics II Viscosity and shear stresses

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

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

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

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


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

Formulae that you may or may not find useful. E v = V. dy dx = v u. y cp y = I xc/a y. Volume of an entire sphere = 4πr3 = πd3

MULTIPLE-CHOICE PROBLEMS:(Two marks per answer) (Circle the Letter Beside the Most Correct Answer in the Questions Below.)

Introduction and Fundamental Concepts (Lectures 1-7)

UNIT I FLUID PROPERTIES AND STATICS

2, where dp is the constant, R is the radius of

CENG 501 Examination Problem: Estimation of Viscosity with a Falling - Cylinder Viscometer

BACHELOR OF TECHNOLOGY IN MECHANICAL ENGINEERING (COMPUTER INTEGRATED MANUFACTURING)

Polymerization Technology Laboratory Course

AMME2261: Fluid Mechanics 1 Course Notes

) = slugs/ft 3. ) = lb ft/s. ) = ft/s

Fluid Mechanics Introduction

Fluid Mechanics Discussion. Prepared By: Dr.Khalil M. Al-Astal Eng.Ahmed S. Al-Agha Eng.Ruba M. Awad

Chapter 1 INTRODUCTION

PHYSICAL MECHANISM OF CONVECTION

Modelling of dispersed, multicomponent, multiphase flows in resource industries. Section 3: Examples of analyses conducted for Newtonian fluids

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

Lecture 3. Properties of Fluids 11/01/2017. There are thermodynamic properties of fluids like:

Welcome to MECH 280. Ian A. Frigaard. Department of Mechanical Engineering, University of British Columbia. Mech 280: Frigaard

ME3560 Tentative Schedule Spring 2019

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

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

Fluid Properties and Units

ME3560 Tentative Schedule Fall 2018

Fluid Mechanics. du dy

Fluid Dynamics for Ocean and Environmental Engineering Homework #2 Viscous Flow

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

Lecturer, Department t of Mechanical Engineering, SVMIT, Bharuch

University of Washington Department of Chemistry Chemistry 453 Winter Quarter 2013

MULTIPLE-CHOICE PROBLEMS :(Two marks per answer) (Circle the Letter Beside the Most Correct Answer in the Questions Below.)

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

ACE Engineering College

Candidates must show on each answer book the type of calculator used. Only calculators permitted under UEA Regulations may be used.

MECHANICAL PROPERTIES OF FLUIDS:

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

S.E. (Mech.) (First Sem.) EXAMINATION, (Common to Mech/Sandwich) FLUID MECHANICS (2008 PATTERN) Time : Three Hours Maximum Marks : 100

Fluid Mechanics-61341

Design and Modeling of Fluid Power Systems ME 597/ABE Lecture 7

FLUID MECHANICS. Gaza. Chapter CHAPTER 44. Motion of Fluid Particles and Streams. Dr. Khalil Mahmoud ALASTAL

Chapter 3 Non-Newtonian fluid

(Refer Slide Time: 0:35)

MECHANICAL PROPERTIES OF FLUIDS

Tutorial 10. Boundary layer theory

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

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

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

Modelling of dispersed, multicomponent, multiphase flows in resource industries Section 4: Non-Newtonian fluids and rheometry (PART 1)

2 Navier-Stokes Equations

Shell Balances in Fluid Mechanics

BFC FLUID MECHANICS BFC NOOR ALIZA AHMAD

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

Prof. Scalo Prof. Vlachos Prof. Ardekani Prof. Dabiri 08:30 09:20 A.M 10:30 11:20 A.M. 1:30 2:20 P.M. 3:30 4:20 P.M.

Iran University of Science & Technology School of Mechanical Engineering Advance Fluid Mechanics

DIMENSIONS AND UNITS

PROPERTIES OF FLUIDS

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

Fluid Mechanics Qualifying Examination Sample Exam 2

Lagrangian description from the perspective of a parcel moving within the flow. Streamline Eulerian, tangent line to instantaneous velocity field.

Flux - definition: (same format for all types of transport, momentum, energy, mass)

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

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

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

Introduction to Micro/Nanofluidics. Date: 2015/03/13. Dr. Yi-Chung Tung. Outline

HYDRAULICS STAFF SELECTION COMMISSION CIVIL ENGINEERING STUDY MATERIAL HYDRAULICS

Exercise: concepts from chapter 10

Fundamentals of Fluid Mechanics

Lecture 2 Flow classifications and continuity

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

Fluid Mechanics Testbank By David Admiraal

Solution to phys101-t112-final Exam

MAHALAKSHMI ENGINEERING COLLEGE TIRUCHIRAPALLI

INTRODUCTION TO FLUID MECHANICS June 27, 2013

CHAPTER 28 PRESSURE IN FLUIDS

V (r,t) = i ˆ u( x, y,z,t) + ˆ j v( x, y,z,t) + k ˆ w( x, y, z,t)

The Bernoulli Equation

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

Introduction to Heat and Mass Transfer. Week 9

6. Basic basic equations I ( )

The most common methods to identify velocity of flow are pathlines, streaklines and streamlines.

BME-A PREVIOUS YEAR QUESTIONS

Fluid Dynamics Midterm Exam #2 November 10, 2008, 7:00-8:40 pm in CE 110

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

Fluid Mechanics Abdusselam Altunkaynak

Transcription:

MM303 FLUID MECHANICS I PROBLEM SET 1 (CHAPTER ) FALL 018 1) For the velocity fields given below, determine: i) Whether the flow field is one-, two-, or three-dimensional, and why. ii) Whether the flow is steady or unsteady, and why bt a) V ax e i V ae i bx j bx b) c) V ax t i by j d) V axy i byztj NOTE: The quantities a and b are constants. ) The velocity field V=axyi+by j, where a= 1/m s, b=-6 1/m s, and the coordinates are measured in meters. Calculate the velocity at the point (, ½). Find an expressionfor for the streamline passing through this point. Plot several streamlines in the first quadrant, including the one passes through the point (x,y)=(,1/) Solution: At point (, ½), the velocity components are u=axy= 1/= m/s v=by =-6 (1/) = -3/ m/s Steamline is tangent to the velocity vector. Hence, for streamline, dy v by by dx u axy ax Separating the variables, dy y bdx ax Integrating, we get, b ln( y) ln( x) c y Cx y Cx a ba / 3 The streamline passing through point (,1/) is obtained as 1 3 1 3 4 C C C 4 y 3 x

3) Velocity field of a flow is given as V=Axi+Ayj, where A= s -1. Verify that the parametric equations for particle motion are x p=c 1e At and y p=c e At. Obtain the equation for the pathline of the particle located at the point (x,y)=(,) at time t=0. Compare the pathline with the streamline through the same point. Solution: dx dx dx 1 1 For pathlines up Ax Adt ln( x) At c1 x e x e e C1e dt dt x dy dy dy At c c At At vp Ay Adt ln( y) At c y e y e e Ce dt dt y At c c At At At Hence the parametric equations of the motion are x C1e and y C e At Equation of the pathlines can be obtained by combining the parametric equations as follows: x C1e e subtituting this into the following equation, we get, C At At x x y C e y C y Cx 1 At C1 y 1 At point (,), C. x The path line of the particle at point (,) at time t=0 is y 1 x For streamline, dy v Ay y dx u Ax x Separating the variable and integrating, we get, dy dx y int egrating ln( y) ln( x) c ln c y Cx y x x y 1 At point (,), C. x The steamline passing through point(,) is y 1 x The streamline passing through point (,) and the pathine that started at point (,) coincide because the flow is steady.

4) Velocity field of a flow is given by V=ai+bxj, where a= 3 m/s and b= s -1. Coordinates are measured in meters. a) Obtain the equation for the streamline passing through point (, 4). b) At t=5 s, what are the coordinates of the particle that passed through point (0, 4) at time t=0 s? c) What conclusion can you draw about the pathline, streamline and streakline for this flow?

5) Crude oil, with specific gravity SG=0.85 and viscosity =0.1 Ns/m, flows steadily down a surface inclined =45 0 in a film of thickness h=.5 mm. The velocity profile is given by the expression below. (Coordinates x is along the surface and y is normal to the surface.) Plot the velocity profile. Determine the magnitude and direction of the shear stress that acts on the surface. u = ρg y (hy ) sinθ μ

6) A block weighing 45 N and having dimensions 50 mm on each edge is pulled up on an inclined surface on which there is a film of SAE 10W oil at 37 0 C. If the speed of the block is 0.6 m/s and the oil film is 0.05 mm thick, find the force required to pull the block. Assume that velocity profile in the oil film is linear. The surface is inclined at an angle of 5 0 from the horizontal.

7) A concentric cylinder viscometer is driven by a falling mass M=0.0 kg connected by a cord and pulley to the inner cylinder, as shown. The liquid to be tested fills the annular gap of width a=0.4mm and height H=160 mm. After a brief starting transient, the mass falls at constant speed V m=60 mm/s. Develop an algebraic expression for the viscosity of the liquid in the device in terms of M, g, V m, r, R, a and H. Evaluate the viscosity of the liquid. Note: r=50 mm, R=100 mm.

8. At a depth of 7.5 km in the ocean, the pressure is 75 Mpa. Assume a specific weight of 10 KN/m 3 at the surface and an average bulk modulus of elasticity of.5 GPa for that pressure range. Find (a) the change in specific volume between the surface and 7.5 km depth, (b) the specific volume at 7.5 km (c) the specific weight at 7.5 km. Solution: Pressure at 7.5km (P ) = 75 Mpa = 75x106 N/m Specific weight at the surface (γ)= 10 KN/m 3 = 10x1000 = 10000 N/m 3 Bulk modulus of elasticity at the surface (E v) =.5 GPa =.5x109 N/m a) Density at the surface (ρ 1 ) = 10000/9.81 = 1019.4 kg/m 3 Specific volume at the surface (v s1)= 1/ρ 1 =1/1019.4=0.000981 m 3 /kg Bulk modulus in terms of specific volume is Ev = P V s V s1

.5 10 9 = 7.5 106 0 V s 0.000981 V s = 0.000094 m 3 /kg b) v s = v s1 + V s = 0.000981-0.000094 = 0.000951 m 3 /kg c) Density at 7.5 km (ρ ) = 1/v s = 1051.5 kg/m 3 γ = ρ g = 1051.5 9.81 = 10315 N/m 3 9. In a fluid the velocity measured at a distance of 75 mm from the boundary is 1.15 m/s. The fluid has a dynamic viscosity of 0.048 Ns/m and a specific gravity (SG) of 0.9. What is the velocity gradient and the shear stress at the boundary assuming a linear velocity distribution. Also calculate the kinematic viscosity. Solution: Assumptions: The fluid is Newtonian The velocity profile is linear Change in velocity ( u) =1.15-0 = 1.15 m/s Change in distance ( y) = 75 0 = 75 mm = 75/1000 m = 0.075 m Dynamic viscosity (µ) = 0.048 Ns/m specific gravity (SG)= 0.9 velocity gradient (du/dy) =? Shear stress (τ ) =? Kinematic viscosity (v) =? Velocity gradient on the boundary can be calculated as du/dy= u/ y=1.15/0.075=15 1/s τ = μ du = 0.048 15 = 0.7 N/m dy Densitiy of fluid= SGxρ water =0.9x1000=900 kg/m 3

v = μ ρ = 0.048 900 = 5.3x10 5 m /s 10) A piston of weight 90 N slides in a lubricated pipe. The clearance between piston and pipe is 0.05 mm. If the piston decelerates at a rate of 0.6 m/s when its speed is 0.5 m/s, what is the viscosity of the oil? Solution: Assumptions: - The oil is Newtonian - Velocity of the oil in the gap is linear. Weight of piston (W) = 90 N Clearance ( y)= 0.05 mm = 0.00005 m Deceleration (a) = 0.6 m/s Change in velocity ( u) = 0.5 m/s Diameter of piston (D) = 15 mm = 0.15m Length of piston (L) = 130mm = 0.13 m Viscosity of oil (µ) =? Frictional force acting on piston (F) = Shear stress(τ) at the piston surface x surface area of piston(a) F = μ du dy (πdl) = μ 0.5 (πx0.15x0x13) = 101x0μ 0.00005 Note: Since velocity profile in the gap is linear, on the piston surface du/dy= u/ y Applying Newtons secon la to the piston, we can write W F = W g a 90 1010.0μ = 90 9.81 ( 0.6) μ = 0.094 Ns/m 11) A flat plate 0.3 m in area moves horizantally through oil between two large fixed parallel walls. The distance between the walls is 10 cm. If the velocity of the moving plate is 0.6 m/s and the oil has a kinematic viscosity of 0. 45 10 4 m /s and specific gravity 0.8, calculate the drag force when

(a) the plate is.5 cm from one of the walls and ( y1=.5). (b) the plate is equidistant from both the walls( y1= y). Solution Assumptions - The oil is Newtonian. - The velocity profile between the moving plate and the stationary walls is linear. a) y1 =.5 cm = 0.05 m y = 10-.5 = 7.5 cm = 0.075 m Total force (F) = Force on side1 (F1) + Force on side (F) = τ1 A + τ A b) If the plate is equidistant, y1 = y = y = 10/ = 5 cm = 0.05 m Total force (F) = Force on side1 (F1) + Force on side (F) = τ1 A + τ A = (τ1 + τ) A 1) The tip of glass tube with an internal diameter of mm is immersed to a depth of 1.5 cm into a liquid of specific gravity 0.85. Air is forced into the tube to form a spherical bubble just at the lower end of the tube. Estimate surface tension of liquid if the pressure in the bubble is 00 Pa.

Solution: Radius of bubble (r) = 1 mm = 0.001m Pressure inside bubble (Pi) = 00 Pa Depth of liquid (h) = 1.5 cm = 0.015 m Specific weight of liquid= SGxγ water = 0.85x9810 = 8338.5 N Surface Tension (σ)=? Pressure outside the bubble (P o) = x h= 8338.4x0.015 = 15.07 Pa The difference between the pressure in the bubbleoutside of the bubble ( P) = 00-15.07 = 74.93 Pa The force actin on the surface of the bubble due this pressure difference is balanced by the surface tension force. Hence we can write dp = σ r σ = dpr = 0.0375 N/m