CE 466 FE Exam Review

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CE 466 FE Exam Review

Fluids

Spring 2013

Overview

Topics:

• Flow measurements

• Fluid properties

• Fluid statics

• Energy, impulse-momentum equations (fluid dynamics)

• Pipe and other internal flow

• Similitude

Basic Definitions

Density = ρ = mass / unit volume (kg/m 3 , slugs/ft 3 )

ρ water

= 1000 kg/m 3 = 1.94 slugs/ft 3

Specific weight = γ = weight / unit volume (N/m 3 , lb/ft 3 )

γ water

= 9810 N/m 3 = 62.4 lb/ft 3

Specific gravity = SG = ρ fluid

/ ρ water

= γ fluid

/ γ water

Basic Definitions (cont.)

Pressure = force per unit area (N/m 2 , psi) gage pressure = measured pressure with respect to atmospheric pressure absolute pressure = measured pressure with respect to absolute zero pressure (complete vacuum) atmospheric pressure = 101 KN/m 2 = 14.7 psi

So P absolute

= P gage

+ P atmosphere

Basic Definitions (cont.)

Stress = force per unit area (N/m 2 , psi) normal stress = area resisting stress is perpendicular

(normal) to force tangential (shear) stress = area resisting stress is parallel to force

Basic Definitions (cont.)

Fluid viscosity = measure of its resistance to flow when acted upon by an external force such as a pressure gradient or gravity

Newton’s law of viscosity: τ = µ dV/dY

Basic Definitions (cont.)

Absolute viscosity: µ = τ δ / V (N • s/m 2 or lb • s/ft 2 )

Kinematic viscosity: υ = µ / ρ (m 2 /s or ft 2 /s)

Basic Definitions (cont.)

Cohesive force = attraction of liquid molecules to each other

Adhesive force = attraction of liquid molecule to a another surface

Surface tension = force that holds a droplet of some fluid together at the fluid/gas interface (cohesive forces greater than adhesive forces towards gas)

Capillary action = attraction of some fluid to a solid surface

(adhesive forces greater than cohesive forces)

Basic Definitions (cont.)

σ = surface tension, N/m or lb/ft

ß = angle of contact

Example 1

Example 1 - Solution

From Kaplan

Example 2

Example 2 - Solution

From Kaplan

Example 3

Fluid Statics

Hydrostatic pressure p acting at some depth h

• p = ρ g h =

γ

h

• same magnitude in all directions

• pressure on a surface will act normal to the surface

Center of Pressure

Y r

F r

F r

= P c

A = γ h c

A

Y r

= Y c

+ I xc

/ (Y c

A)

Y c

Magnitude of resultant force is equal to pressure of centroid of surface x surface area

Result force acts at the centroid of the pressure distribution,

NOT centroid of surface!

Example 4

What is the resultant force on a the end of a square tank measuring

20 ft x 20 ft and containing 10 ft of water, and where does the resultant force act?

F r

h = 10 ft

w = 20 ft

Example 4

Pressure Prism with height of 10 m and width of 20 m.

Pressure distribution is 0 at top to 624 lb/ft 2 ( γ x h) at bottom

Resultant force = Volume of pressure-area prism

= ½ base x h x w

= (1/2) (624 lb/ft 2 ) (10 ft) (20 ft) = 62,400 lb

Acts at centroid of prism (not surface)

= 1/3 h up from the bottom = 10 ft / 3 = 3.33 ft

= 1/2 w over = 20 ft / 2 = 10 ft

Pressure Measurements

From Ref Hdbk

Example 5

Based on the manometer readings shown in the figure, what is the pressure in water pipe?

Example 5 - Solution p pipe

= γ m h m

- γ w h w

γ m h m

= (2.0 ft) (13.6) (62.4 lb/ft 3 ) = 1297 lb/ft 2

γ w h w

= (1.5 ft) (62.4 lb/ft 3 ) = 94 lb/ft 2 or water pressure in pipe = p pipe

= 1203 lb/ft 2 = 8.4 psi

Buoyancy

F

B

=

γ

f

V

D

F

B

= buoyancy force

γ

f

= specific weight of fluid

V

D

= volume displaced by an object

A body immersed in a fluid is buoyed up by a force equal to the weight of fluid displaced.

A floating body displaces its own weight of the liquid in which it floats.

Example 6

Example 7

Example 7 - Solution

Fluid Dynamics

Conservation of mass:

mass entering system = mass exiting system

ρ

1

A

1

v

1

= ρ

2

A

2

v

2

; mass flow rate in kg/s or lbm/s

For incompressible fluids: ρ

1

= ρ

2

A

1

v

1

= A

2

v

2

With Q = volumetric flow rate = A v in m 3 /s or ft 3 /s

Q

1

= Q

2

Example 8

Example 8 - Solution

Fluid Dynamics (Cont.)

Fluid energy - expressed in terms of head (m or ft)

velocity head = v 2 / (2g) pressure head = P/ γ elevation head with respect to a reference datum = z

Hydraulic grade line = pressure head + elevation head

Energy grade line = pressure head + elevation head + velocity head

See handout.

Fluid Dynamics (Cont.)

Conservation of energy (Bernoulli equation):

Final = Initial – losses + gains p

2

/ γ + v

2

2 /2g + z

2

= p

1

/ γ + v

1

2 /2g + z

1

– h f

– h f,fittings

– h t

+ h p

h f

= head loss from friction (“major headloss”)

h f,fittings

= friction losses at fittings, bends, contractions and expansions on right (“minor headloss”). See Reference

Handbook. h f,fittings

= Cv 2 /2g; C ~0.1-2.0

h t

= head removed due to a turbine

h p

= head added due to a pump

Example 9

Example 9 - Solution

From Kaplan

BREAK

Friction Losses

Friction loss for low of velocity v in a pipe of length L and diameter D ( Darcy-Weisbach equation) : h f

= f L/D v 2 /2g f = Darcy friction factor

Look up f as a function of R e

and ε/D on Moody diagram.

Use this equation to estimate hf and plug it into Energy Equation.

See handout – 3 rd to last page!

Pump Power and Efficiency

W = γ Q h p

/ η

W = pump power (N-m/s = J/s = watt; ft-lb/sec, 550 ftlbf/sec = 1 horsepower or hp); η = pump efficiency (~0.7); h p

= pump head in m or ft

Moody Diagram Calculation

TAPS Problem

See Handout

Parallel Pipe Flow

Head loss in each branch will be the same: f

A

L

A

/D

A

v

A

2 /2g = f

B

L

B

/D

B

v

B

2 /2g

Total flow in must equal flow in two branches: Q = Q

A

+ Q

B

Reynolds Number

Unitless or non-dimentional numbers

Re = inertial forces / viscous forces = ( ρ v L ) / μ

For pipe flow Re = ( ρ v D ) / μ where D is pipe diameter

Laminar flow if Re < 2100

Turbulent flow if Re > 4000

Transitional flow in between

Impulse-Momentum

Σ F = ρ Q (v out

– v in

)

May need to consider forces in 1, 2 or 3 directions (treat as vectors, or treat as scaler and handle geometry)

Forces will develop in pipe bends, deflectors, blades

-- see Reference Handbook

Example 11

F z

= ?

Example 11 - Solution

(V z-out

– V z-in

)

(50 – 0 m/s)

Example 12

Example 12 - Solution

Fluid Flow Measurements – Pitot Tube

V = (2 g h) 1/2

From Ref Hdbk

Fluid Flow Measurements – Orifices

From Ref Hdbk

Fluid Flow Measurements – Submerged Orifice

From Ref Hdbk

Fluid Flow Measurements – Freely Discharging

Orifice

From Ref Hdbk

Dimensional Analysis

Dimensionally homogeneous equation = equations that do not depend on the units of measurement

Example: Flow in pipes dominated by viscosity and inertia

Re = ( ρ v D ) / μ

To conduct a test on a scaled model for pipe model (m) and prototype (p):

[( ρ v D ) / μ ] m

= [( ρ v D ) / μ ] p

Similitude

A model must be geometrically, kinematically and dynamically similar to the prototype

For a phenomenon involving n variables consisting of r dimensions (mass, length, time, temp, etc.), then ( n – r ) independent dimensionless groups (referred to as π groups) are needed to properly model the behavior of the prototype = similitude requirements

Example 13

Example 14

Example 14 - Solution

From Kaplan

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