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CFD MODEL OF A SPINNING PIPE GAS LENS

SAIP

Dr Andrew Forbes July 2006

G Snedden 1 , A Forbes 2 , C Mahlase 1 , C Mafusire 3 and MM Michaelis 4

1

CSIR DPSS, PO Box 395, Pretoria

2

CSIR National Laser Centre, PO Box 395, Pretoria

3

University of Zimbabwe, Mount Pleasant, Harare

4

University of Kwazulu-Natal, Durban

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Spinning Pipe Gas Lens

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Page 3

© CSIR 2006 www.csir.co.za

Focal Length

78 C:f = 94.655w-1.1388 104 C:f = 138.94w-1.4796 125 C:f = 79.151w-1.3439 152 C:f = 197.55w-1.7476

0 1 2 3 4 5 6 7 8 9

6 8 10 12 14 16 18 20

Pi pe Spe ed,w (Hz )

Focal Length, f (m)

T =78 C T =104 C T =125 C T =152 C Power (T =78 C) Power (T =104 C) Power (T =125 C) Power (T =152 C)

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Refractive Index

1.0002 1.00021 1.00022 1.00023 1.00024 1.00025 1.00026 1.00027 1.00028 1.00029 1.0003 1.00031

-20 -15 -10 -5 0 5 10 15 20

Radial Distance, r(mm)

Refractive Index, n(r)

78 C 104 C

125 C 153 C

Poly. (78 C) Poly. (104 C) Poly. (125 C) Poly. (153 C)

(5)

Gas Dynamics

(6)

Cold Air

Warm Air

Cold Air

Warm Air Warm Air Tube Rotation

Heater tape Warm

Air Opposing Vortices

Guess at the gas dynamics

(7)

Page 7

© CSIR 2006 www.csir.co.za

Density Profile

(8)

Density Profile

(9)

Page 9

© CSIR 2006 www.csir.co.za

Flow Profile

(10)

Rosby Waves

(11)

Page 11

© CSIR 2006 www.csir.co.za

Rayleigh–Taylor Instabilities

(12)

Future Work

(13)

Page 13

© CSIR 2006 www.csir.co.za

Instabilities near the boundary

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3 / 5

0

2

 

= N

nm

D r σ

nm

) 6 / 23 (

) 6 / 17 (

) 6 / 5 ( ) 3 / 14 ( ) 1 ( ) 1 ( 15337 .

0

2

Γ +

Γ

− Γ Γ

+

= −

n

n N n

m n nm

∑ ∑

= =

+

= Φ

0 0

)]

, ( )

, ( [

) , (

n n

m

m n m n m

n m

n U B V

A ρ θ ρ θ

θ ρ

∫ ∫ Φ

= +

π

ρ θ ρ θ ρ ρ θ π

2 0

1

0

( , ) ( , )

) 1

( n U d d

m K

A

nm nm

=

+

− −

=

2

0

2 2

2

)! ( )!

(

!

)!

( ) 1 ) (

(

m n

k

k n m

n m

n k m

n

k k k

k

R ρ n ρ

3 / 5 2

2 0

max

min

) ( 423

. 0

 

 

=  ∫

h

h

n

h dh C

k r

Wavefront Measurement & Control

(15)

Page 15

© CSIR 2006 www.csir.co.za

Adaptive optics for turbulence correction

• SLM acts as an adaptive optic

• Measure wavefront distortion,

• Feed result back into SLM to create conjugate phase,

• Propagate conjugate phased beam through medium.

Control Loop

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Conclusion

• CFD model of gas lens

• Shows Rosby waves and Rayleigh–Taylor instabilities

• Propagation model in preparation

• Full Fresnel propagation through GRIN system

• Future work

• Adaptive optics theory and experiment

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Questions

Referensi

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