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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  

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