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Lecture 3 Kinematics (2)

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Lecture 3

Kinematics (2)

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Contents

3.1 Flow Lines

3.2 Differential Equations of Flow Lines

3.3 One-, Two-, and Three-Dimensional Flows

Objectives

- Classify flow lines

- Study equation of streamline

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3.1 Flow Lines

3.1.1 Flow lines

3 flow lines: streamline, path line, streak line (1) streamline

= imaginary line connecting a series of points in space at a given instant in such a manner that all particles falling on the line at that instant have

velocities whose vectors are tangent to the line

= instantaneous curves which are everywhere tangent to the velocity vector

= a line that is (at a given instant) tangent to the velocity at every point on it

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3.1 Flow Lines

Dense streamline → high velocity, low pressure

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3.1 Steady and Unsteady Flow, Streamlines, and Streamtubes

Source and Sink

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~ may be treated as if isolated from the adjacent fluid

~ many of the equations developed for a small stream tube will apply equally well to a streamline.

3.1 Steady and Unsteady Flow, Streamlines, and Streamtubes

• Stream tube (유관)

~ aggregation of streamlines drawn through a closed curve in a steady flow forming a boundary across which fluid particles cannot pass because the velocity is always tangent to the boundary

No flow in and out

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* stream tube = small imaginary tube bounded by streamlines

* stream filament = if cross section of stream tube is infinitesimally small

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3.1 Flow Lines

(2) path line

= trajectory of a particle of fixed identity as time passes

(3) streak line

= a line connecting all the particles that have passed successfully through a particular given (common) point (injection point)

= current location of all particles which have passed through a fixed point in space

[Ex] dye stream in water, smoke filament in air

* For steady flow, streamline = path line = streak line

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◈ How can we photo 3 lines?

(1) streamline: spread bunch of reflectors on the flow field, then take a instant shot

(2) path line: put only one particle on the flow field, then take long-time exposure

(3) streak line: take a instant shot of dye injecting from one slot of the dye tanks

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3.1 Flow Lines

Streak line by LIF Path line by PIV

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Streamline + Path line

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3.1 Flow Lines

At low velocity

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At high velocity

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3.2 Differential Equations of Flow Lines

q

xy

dy

v dx u

3.2.1 Differential equations for flow lines

(1) Equation of streamline

By virtue of definition of a streamline (velocity vector is tangent to the streamline), it’s slope in the - plane, , must be equal to that of the velocity, .

dy v

dxu

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dz w ;

dxu dz w

dyv

dx dy dz

uv w

 

By similarly treating the projections on the xz plane and on the yz plane

→ Integration of the differential equation for streamline yields equation of streamline. For 2-D Cartesian coordinates

dx dy dy v 0

v dx udy

uvdxu   

(3.1)

(3.2)

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3.2 Differential Equations of Flow Lines

3.2.2 Streamline coordinates

Consider one-dimensional flow in a streamline coordinates (유선좌표계)

Select a fixed point 0 as a reference point and define the displacement of a fluid

particle along the curved streamline in the direction of motion.

→ In time dt the particle will cover a differential distance ds along the streamline.

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v ds

dt 1) Velocity,

- magnitude of velocity:

where s = displacement (변위)

- direction of velocity: tangent to the streamline

as

ar

2) Acceleration,

- acceleration along (tangent to) the streamline = - acceleration outward normal to the streamline =

v

a

s r

aa sa r

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3.2 Differential Equations of Flow Lines

s

dv dv ds dv

a v

dt ds dt ds

  

2 r

a v

  r ← particle mechanics

r s

where = radius of curvature of the streamline at

(3.3) (3.4)

2

s n

a a s a n dv v

v s n

ds r

 

 

[Re] Circular motion

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(2) Path line

Since the particle is moving with the fluid at its local velocity

dx ;

dtu dy ;

dtv dz

dtw

(3.5)

[Ex] A fluid flow has the following velocity components;

Find an equation for the streamlines of this flow.

1 / , 2 / . um s vx m s

2 1 dy v x dx  u

yx

2

c

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3.2 Differential Equations of Flow Lines

[Re] Vector form of equation of streamline 0

qdr

qiujvkw

dri dxj dyk dz

n ds  element of length along streamline

qdrivdzjwdxkudyiwdyjudzkvdx

( ) ( ) ( ) 0

i vdz wdy j wdx udz k udy vdx

      

(3.6)

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 Vector Products

(1) dot product → scalar

1 1 2 2 3 3

a b   a ba ba b

(2) cross product → vector

     

1 2 3

1 2 3

2 3 3 2 3 1 1 3 1 2 2 1

i j k

a b a a a

b b b

a b a b i a b a b j a b a b k

 

     

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Appendix

i j k

curl V V

x y z

u v w

  

   

  

w v u w v u

i j k

y z z x x y

           

                       

Sarrus’ rule

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[Ex] Vorticity: v u

x y

  3–D flow,

   V

For irrotational flow,

 0 ;   V  0

( ) ( )

curl uv    uv       u v u v 0

curl grad u      u

  0

divcurl u      u

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3.3 One-, Two-, and Three-Dimensional Flows

• One-dimensional flow

~ All fluid particles are assumed uniform over any cross section.

~ The change of fluid variables perpendicular to (across) a streamline is negligible compared to the change along the streamline.

~ powerful, simple

~ pipe flow, flow in a stream tube

- average fluid properties are used at each section

( ) Ff x

Actual velocity

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• Two-dimensional flow

~ flow fields defined by streamlines in a single plane (unit width)

~ flows over weir and about wing

~ assume end effects on weir and wing is negligible

( , )

vf x z

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3.3 One-, Two-, and Three-Dimensional Flows

• Three-dimensional flow

~ The flow fields defined by streamlines in space.

~ axisymmetric three-dimensional flow

→ streamlines = stream surfaces

( , , )

vf x y z

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Homework Assignment No. 1 Due: 1 week from today

3

1 3 s

q ui u R i

x

 

    

 

3 ,

x   R x  2 ,R x  R What is the fluid acceleration at (a) (b) and (c) ?

2 / usm s

2 x   R

(d) When and and R = 3 cm, what is the magnitude of the acceleration at ?

1. The velocity of an inviscid, incompressible fluid as it steadily approaches the stagnation point at the leading edge of a sphere of radius R is

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Problems

2. The velocity field in a flow system is given by

5 ( 2) 3

qixy jxy k

What is the fluid acceleration (a) at (1, 2, 3) and (b) at (-1, -2, -3)?

3. A nozzle is shaped such that the axial-flow velocity increases linearly from 2 to 18 m/s in a distance of 1.20 m. What is the convective acceleration (a) at the inlet and (b) at the exit of the nozzle?

4. Determine the streamline for the two-dimensional steady flow given by

where V0 and l are constants. Plot it.

0 ( )

q V xi yj

l  

참조

관련 문서

• In any flow of a barotropic inviscid fluid, the circulation about any closed path does not vary with time if the contour is imagined to move with the fluid, that is, always to

For irrotational flow of ideal incompressible fluid, the Bernoulli’s equation applies over the whole flow field with a single energy line. Exact velocity field

~ a volume which is fixed in space and through whose boundary matter, mass, momentum, energy can flow. ~ The boundary of control volume is

• Mechanism of boundary layer growth on a smooth flat plate - Boundary layer flow: laminar → transition → turbulent - Velocity of the fluid particle at the body wall is

~ In steady flow, Lagrangian path lines are the same as the Eulerian streamlines, and both are the same as the streak lines, because the streamlines are then fixed in space

7.2 Turbulent Flow and Eddy Viscosity 7.3 Fluid Flow Past Solid Boundaries 7.4 Characteristics of Boundary Layers 7.5 The Laminar Boundary Layer*.. 7.6 The

- Turbulence is generated primarily by friction effects at solid boundaries or by the interaction of fluid streams that are moving past each other with different velocities

7.2 Turbulent Flow and Eddy Viscosity 7.3 Fluid Flow Past Solid Boundaries 7.4 Characteristics of Boundary Layers 7.5 The Laminar Boundary Layer*.. 7.6 The