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A Study on the Roton-limited Thermal Boundary Shock Wave in Liquid Helium Films

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A Study on the Roton-limited Thermal Boundary Shock Wave in Liquid Helium Films

Chul-Won Jun

School of Mechanical Engineering, Kyungnam University, Changwon 631-701, Korea (Received 20 May 2013 : revised 7 June 2013 : accepted 15 July 2013)

The thickness of the roton-limited thermal boundary shock wave in liquid helium films is obtained as a function of temperature by solving the two-fluid hydrodynamic equations including dissipation coefficients. The roton-limited temperature region in liquid helium films with a particle density of 0.0279 ˚ A

−2

is about 0.8 K < T < 1.2 K. In this temperature region, phonon-roton transformation processes and roton-roton scattering processes play the main roles in investigating the temperature variations of the dissipation coefficients. Based on these interactions, the thickness of the thermal boundary shock wave depends on the thermal conductivity, the first viscosity, and the second viscosity, and decreases with increasing temperature. The pressure is also shown to be high on the side of the boundary where the temperature is high while the normal fluid velocity is low on that side.

PACS numbers: 67.40.Pm

Keywords: Thermal boundary shock wave, Two-fluid hydrodynamic equations, Phonon-roton transformation processes, Roton-roton scattering processes

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PACS numbers: 67.40.Pm

Keywords: \ P  â >  Ø  æ   , 2Ä »^ ‰% i † < Æ ~ ½ Ó& ñ d ” , Ÿ í 7 H- – З : r   ¨ 8 Š õ & ñ , – З : r- – З : r í ß –ê ø Íõ & ñ

E-mail: [email protected]

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∂ρ

∂t + ∇ · j = 0 (3)

∂v s

∂t + ∇(µ + 1

2 v 2 s ) = ∇[ζ 3 ∇ · (j − ρv n ) + ζ 4 ∇ · v n ] (4)

∂E

∂t + ∇ · (Q + Q

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) = 0 (5)

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∂t + ∇ · (ρσv n − K

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T (6)

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∂r i

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ρ (v n − v s ) · d(v n − v s ) (8)

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τ ij = − η( ∂v ni

∂r j

+ ∂v nj

∂r i

− δ ij ∇ · v n )

− δ ij [ζ 1 · ρ s (v s − v n ) + ζ 2 ∇ · v n ] (10)

Q = (µ + v S 2

2 )j + ρσT v n + ρ n v n [v n · (v n − v s )] (11)

(3)

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0

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+ζ 3 [∇ · (j − ρv n )] 2 + 1

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∂r i − δ ij ∇ · v n ] 2 + K

T (∇T ) 2 (14)

j = ρ s v s + ρ n v n (15)

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[µ + v s 2

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∂x + ζ 3 v n

∂ρ

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[p + ρ n ρ s

ρ (v n − v s ) 2 − (η + ζ 2 − ρζ 1 ) ∂v n

∂x + ζ 1 v n

∂ρ

∂x ] = 0 (18) [ρσ(T + v n ρ n

ρσ (v n − v s )v n

−K ∂T

∂x − β ∂v n

∂x v n + (ζ 1 − ρζ 3 )v 2 n ∂ρ

∂x ] = 0 (19)

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∆p − (η + ζ 2 − ρζ 1 ) ∂∆v n

∂x = 0 (21)

ρσT ∆v n − K ∂∆T

∂x = 0 (22)

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€

 

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ρ 2 σ 2 T ] 1/2 (25) s

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= ∇[ζ 1 ∇ · (j − ρv n ) + ζ 2 ∇ · v n ], (26)

˙

v s + ∇[µ + v s 2

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µ r \  ‚  + þ A“   † ½ Óë ß –`  ¦ × þ ˜ # Œ

N ˙ r + N r ∇ · v n = −Γ rph µ r (28)

`

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ñ d ” “ É r  6 £ § õ  ° ú   .

˙

ρ + ∇ · j = 0 (29)

(4)

S ˙ r + ∇ · S r v n = 0 (30)

(29)d ” õ  (30)d ” `  ¦ (28)d ” \  @ /{ 9  €   N ˙ r = − ∂N r

∂ρ ∇ · j − ∂N r

∂S r S r ∇ · v n

+ ∂N r

∂ρ ∇ · ρv n − ∂N r

∂ρ ρ∇ · v n . (31) s

 ÷ &“ ¦ (28)d ” õ  (31)d ” `  ¦  6   x # Œ µ r \  @ /K  Û  ¦€     6

£

§ _  d ” `  ¦ % 3   H  .

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"

∂N r

∂ρ ∇ · (j − ρv n ) + ∂N r

∂ρ ρı · v n

#

. (32)

(26)d ” õ  (27)d ” \       H · ú š§ 4  pü <  o† < Æ( J $ ™[ >  µ  H – Ð

—

: r _   o† < Æ( J $ ™[ > \  _ ” > r Ù ¼– Ð

∇p = −∇( ∂p

∂µ r µ r ), ∇µ = −∇( ∂µ

∂µ r µ r ). (33) s

 ÷ &“ ¦ (32)d ” , (33)d ” õ  † < Êa  (26)d ” , (27)d ” “ É r ∇ · v n õ 

∇ · (j − ρv n ) _  e ” _ _  ° ú כ\  @ /K  $ í w n K   Ù ¼– Ð  6 £ § _

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∂N r

∂ρ

"

N r − ∂N r

∂S r

S r − ∂N r

∂ρ ρ

#

, (34)

ζ 2 (T ) = 1 Γ rph

"

N r − ∂N r

∂S r S r − ∂N r

∂ρ ρ

# 2

, (35)

ζ 3 (T ) = 1 Γ rph

"

∂N r

∂ρ

# 2

, (36)

ζ 4 (T ) = − 1 Γ rph

∂N r

∂ρ

"

N r − ∂N r

∂S r

S r − ∂N r

∂ρ ρ

#

(37)

#

Œl " f \ P % i † < Æ › ' a > 

dE = T dS r + µ r dρ − N r dµ r (38)

p = −E + S r T + µ r ρ (39)

  6   x ÷ &% 3 Ü ¼ 9 ζ 4 = ζ 1 Ü ¼– Ð" f î  r1 l x > à º[ þ t _  @ /g A" é ¶ o 

\

 ¦ ë ß –7 á ¤ ô  Ç . (34)d ”  - (37)d ” \       H Ÿ í 7 H- – З : r   ¨ 8 Š õ

& ñ _  î  r1 l x > à º Γ rph   H – З : r à º_     o\  @ /ô  Ç ¢ - a  oõ 

&

ñ `  ¦ “ ¦¹ 1 Ï # Œ % 3 # Q”   . ¢ - a  oõ & ñ `  ¦ “ ¦¹ 1 Ï l  0 A # Œ



 ¨ 8 Š õ & ñ _   © œ  ñ Œ •6   x \  -t \  ¦ δ † < Êà º ( J $ ™[ > – Ð Ò q ty Œ • 

“

¦  © œ  ñ Œ •6   x _  [ jl \  ¦ V 0 , Ÿ í 7 H õ  – З : r _  0 Au  7 ˜' \  ¦ y Œ • y

Œ

• r 1 , r 2   ½ + É M :  © œ  ñ Œ •6   x \  -t   H V = V 0 δ(r 1 −r 2 ) – Ð

³

ð‰ & ³ ) a  . î  r1 l x | ¾ Ó p 1 _  Ÿ í 7 H õ  î  r1 l x | ¾ Ó P 2 _  – З : r s  î  r 1

l

x | ¾ Ó P 3 , P 4 _  – З : r Ü ¼– Ð „  s  | ¨ c S X ‰Ò  ¦`  ¦ dW   €   dW = 2π

~

| V AF | 2 δ( 1 + E 2 − E 3 − E 4 ) P 3 P 4

(2π~) 2 (40)

 ÷ &“ ¦ V AF   H „  s ' Ÿ § > =כ ¹™ è\  ¦    · p . { 9   l ‘ : r[ þ t

>

p

u[ þ t _  Š © œõ  í ß –ê ø Í l ‘ : r[ þ t> p u[ þ t _  Š © œ\    É r › ¸ o  ) a ¨ î €  

\  ¦ 1 l x † < Êà º– Ð × þ ˜ # Œ 0 A_  d ” _  & h ì  r`  ¦ > í ß – €     6

£

§ õ  ° ú   .

Z

| V AF | 2 dP 2

(2π~) 2 = 4 | V 0 | 2 (41)

Ÿ

í 7 H õ  – З : r _  ì  r Ÿ í† < Êà º\  ¦ y Œ •y Œ • n, NÜ ¼– Ð   ? /€   Ÿ í



7 H- – З : r   ¨ 8 Š õ & ñ \    É r – З : r à º_     oÖ  ¦ ˙ N r   H N ˙ r = −

Z

[n 1 N 2 (N 3 + 1)(N 4 + 1)

−(n 1 + 1)(N 2 + 1)N 3 N 4 ]dW dp 1 dP 4

(2π~) 4 (42) s

“ ¦ – З : r ì  r Ÿ í† < Êà º\  @ /ô  Ç / å L à º„  > h\  ¦ : Ÿ x K  0 A_  d ” `  ¦

>

í ß – €  

N ˙ r = µ r − µ ph

KT

16π 2

~c 2

|V 0 | 2 (2π~) 6

Z

N 3 N 4 dP 3 dP 4 (43)

  ) a  . # Œl " f µ r , µ ph   H y Œ •y Œ • – З : r õ  Ÿ í 7 H _   o† < Æ(  J $

™[ > `  ¦   ? / 9 – З : r _  \  -t  Û ¼& 7 ˜à Ô! 3 Ü ¼– РÒ'  P ' P 0 \  ¦  6   x % i  . é ß –0 A€  & h { © œ – З : r _  à º N r “ É r

N r = 1 (2π~) 2

Z

N dP (44) s

Ù ¼– Ð (43)d ” _  & h ì  r`  ¦ ½ ¨ €  

N ˙ r = µ r − µ ph KT

4|V 0 | 2 N r 2 ∆ c 2 ~ 3

(45)

 ÷ &“ ¦ # Œl " f N r “ É r  6 £ § _  “ : r • ¸_ ” > r`  ¦ ”   .

N r = ( m KT 2π ) 1/2 P 0

~ 2

e

KT

(46)

–

З : r à º_     oÖ  ¦ ˙ N r \  ¦ Ÿ í 7 H- – З : r   ¨ 8 Š õ & ñ _  î  r1 l x > à º Γ rph – Ð   ? /€  

N ˙ r = Γ rphr − µ ph ) (47) s

“ ¦ (45)d ” õ  q “ § €   Γ rph   H

Γ rph = 4|V 0 | 2 N r 2

c 2 ~ 3 KT (48)

(5)

 ÷ & 9 (46)d ” `  ¦  6   x † < ÊÜ ¼– Ð" f  6 £ § _  “ : r • ¸_ ” > r`  ¦ % 3   H



.

Γ rph = ae

KT2∆

(49)

#

Œl " f  © œÃ º† ½ Ó`  ¦ a – Ð   ? /% 3  .

\ P

„  • ¸• ¸_  – З : r  Òì  r“ É r  6 £ § _  î  r1 l x ~ ½ Ó& ñ d ”  n

0

kT 2 ∇T · (p ST

ρ n − E ∂E

∂P ) = J (n) (50)

`

 ¦ Û  ¦ # Q   9 # Œl " f n

0

  H ¼ # y Œ •\  @ /ô  Ç • ¸† < Êà ºs “ ¦ J (n)“ É r Ø  æ[  t& h ì  r`  ¦    · p . 0 A_  î  r1 l x ~ ½ Ó& ñ d ” `  ¦ ç ß –é ß – y

 l  0 A # Œ Ø  æ[  t& h ì  r`  ¦ – З : r- – З : r Ø  æ[  t _  ¨ î ç  H r ç ß – t r _  † ½ ÓÜ ¼– Ð æ ¼€   J(n) = −(n − n 0 )/t r – Ð @ /u ½ + É Ã º e ” 

“

¦ \ P „  • ¸• ¸_  – З : r  Òì  r`  ¦ ½ ¨ €    6 £ § õ  ° ú    [11].

K r = t r ∆ 2 N r

2m T

"

1 + 3KT

∆ + 15K 2 T 2 4∆ 2

− 2m S ρ n K

KT

∆ + 3K 2 T 2 2∆ 2

!#

(51)

(51)d ” \       H – З : r- – З : r Ø  æ[  t _  ¨ î ç  H r ç ß – t r “ É r Ÿ í



7 H- – З : r   ¨ 8 Š õ & ñ _  î  r1 l x > à º_  “ ¦¹ 1 Ï õ & ñ õ  Ä »   .

–

З : r- – З : r í ß –ê ø Íõ & ñ _   © œ  ñ Œ •6   x ( J $ ™[ > `  ¦ δ+ þ A ( J $ ™[ > – Ð



 ? /“ ¦ Ä » ô  Ç > í ß –õ & ñ `  ¦ : Ÿ x K  t r `  ¦ ½ ¨ €    6 £ § õ 

° ú    [11].

1

t r = 4m |V 0 | 2 N r

~ 3

(52)

]

j 1& h $ í > à º_  – З : r  Òì  r`  ¦ % 3 l  0 A # Œ r ç ß –\    



  t  · ú §  H Ó  o^ ‰ ó ¡ šµ ¢ § _   r & h “   î  r1 l x`  ¦ Ò q ty Œ • “ ¦ Ó  o

^

‰_  5 Å q • ¸ u_  ~ ½ ӆ ¾ Ó`  ¦ y» ¡ ¤ ~ ½ ӆ ¾ ÓÜ ¼– Ð, 5 Å q • ¸ l Ö  ¦ l _  ~ ½ Ó

†

¾ Ó`  ¦ x» ¡ ¤ ~ ½ ӆ ¾ ÓÜ ¼– Ð × þ ˜ €   ó ¡ šµ ¢ § € 9 2 £ § _  – З : r Ü ¼– Ð ] jô  ǝ ) a ]

j1& h $ í > à º  H  6 £ § _  î  r1 l x ~ ½ Ó& ñ d ” 

n 0 P 0 (P − P 0 ) m KT

∂u

∂x cos θ sin θ = J (n) (53)

`

 ¦ Û  ¦ # Q" f % 3 # Q”   . # Œl " f θ  H P ü < x» ¡ ¤ s  s À ҍ  H y Œ •

`

 ¦    · p . î  r1 l x ~ ½ Ó& ñ d ” `  ¦ ç ß –é ß –y  l  0 A # Œ \ P „  • ¸

•

¸_   â Ä º% ƒ! 3  J(n) = −(n − n 0 )/t r – Ð ¿ º“ ¦ ] j1& h $ í >  Ã

º_  – З : r  Òì  r η r `  ¦ ½ ¨ €    6 £ § õ  ° ú    [11].

η r = t r P 0 2 N r

8m (54)

Fig. 1. Temperature variation of the roton-limited thick- ness of the thermal boundary shock wave.

IV. + s ÇÊ Ý õ m Í À X Ø8 ý

· ú

¡ ] X \ " f  H Ó  o^ ‰ ó ¡ šµ ¢ § € 9 2 £ § \  @ /K  – З : r _  l # Œ

×

 æ כ ¹r  ÷ &  H – З : r ] jô  ǝ ) a “ : r • ¸% ò % i \ " f_  \ P  â >  Ø  æ  

 ¿ ºa  ƒ  ½ ¨÷ &% 3 Ü ¼ 9 ¿ ºa   H \ P „  • ¸• ¸, ] j1& h $ í > à º, ]

j2& h $ í > à ºü < ° ú  “ É r ™ èY > > à º[ þ t \  _ ” > r “ ¦ s [ þ t > à º [

þ

t s   7 H _ ÷ &# Q& ’  . ™ èY > > à º[ þ t _  “ : r • ¸\    É r    o\  ¦

%

3 l  0 A # Œ { 9  x 9 • ¸ 0.0279 ˚ A −2 “   Ó  o^ ‰ ó ¡ šµ ¢ § € 9 2 £ §

\

" f_  B > h  à º[ þ t _  ° ú כ[ þ t – Ð" f a = 4 × 10 49 , ∆/K B = 4.12 K, P 0 = 1.02~ ˚ A −1 , m = 0.75m He , c = 164.4 m/s [11]\  ¦  6   x # Œ – З : r- – З : r í ß –ê ø Í_  : £ ¤$ í r ç ß –`  ¦ ½ ¨ €  

1

t r = 4.99 × 10 −3 T 1/2 e −4.12/T (55)

 ÷ &“ ¦ (54)d ” \  @ /{ 9  €   η r “ É r €  • 59.13Ü ¼– Ð" f “ : r • ¸\  1

l qw n e ” `  ¦ · ú ˜ à º e ”  . \ P „  • ¸• ¸\  @ /ô  Ç (51)d ” õ  ] j2& h 

$ í

> à º\  @ /ô  Ç (34)d ”  - (37)d ” “ É r (49)d ” , (55)d ” õ  † < Êa 

\ P

% i † < Æ   à º[ þ t _  “ : r • ¸_ ” > r`  ¦  6   x # Œ ½ ¨ €  

K r = 6.61 × 10 9

"

1

T + 0.22T + 0.73 − 4.74( 1

T + 0.36)

×

( 1 + 28.02(1.5 + 4.12 T )T −1.5 e −4.12/T 1 + 4632.89T −3.5 e −4.12/T

)#

(56)

ζ 1 (T ) = 13.82 × 10 −12 T (10.92 − 11.33T −1 ) 2

×



1 + 4.12

(0.75 + 4.12T −1 + 16.97 × T −2 )(10.92T − 11.33)



(57)

(6)

ζ 2 (T ) = 25.64 × 10 −21 T (10.92 − 11.33T −1 ) 2

×



1 + 4.12

(0.75 + 4.12T −1 + 16.97 × T −2 )(10.92T − 11.33)

 2 (58)

ζ 3 (T ) = 7.45 × 10 −3 T (10.92 − 11.33T −1 ) 2 (59)

ζ 4 (T ) = ζ 1 (T ) (60) s

  ) a  .   " f Ó  o^ ‰ ó ¡ šµ ¢ § € 9 2 £ § \ " f_  \ P % i † < Æ   à º[ þ t õ

 † < Êa  0 A_  ™ èY > > à º[ þ t`  ¦ \ P  â >  Ø  æ    ¿ ºa \  @ /ô  Ç (25)d ” \  @ /{ 9  # Œ • ¸r  €   Fig. 1õ  ° ú   . { 9  x 9 • ¸

0.0279 ˚ A −2 “   Ó  o^ ‰ ó ¡ šµ ¢ § € 9 2 £ § \ " f_  e ” > “ : r • ¸  H 1.2 K s

“ ¦ ™ èY > > à º[ þ t \  @ /ô  Ç – З : r _  l # Œ ×  æ כ ¹r ÷ &  H “ : r

•

¸% ò % i \ " f \ P  â >  Ø  æ    ¿ ºa δ  H “ : r • ¸ 7 £ x † < Ê\   



 y Œ ™™ èô  Ç . & ñ  © œ  â >  # 4 Ü ¼– РÒ'  Ó  o^ ‰ ó ¡ šµ ¢ § Ü ¼– Ð \ P â ì 2

£

§ s  { 9 # Q± ú ˜ M : \ P â ì2 £ §“ É r  â > \ " f Ô  ¦ƒ  5 Å q Ü ¼– Ð    

“

¦ (24)d ” õ  ° ú  s  t à º& h Ü ¼– Ð y Œ ™û Z   H q „    1 l x+ þ A I

_  Ø  æ   – Ð" f ³ ð‰ & ³ ) a  . ¢ ¸ô  Ç (24)d ” `  ¦  6   x † < ÊÜ ¼– Ð" f (20)d ” -(22)d ” Ü ¼– РÒ'  “ : r • ¸    o\    É r & ñ  © œÄ »^ ‰ 5 Å q • ¸



  o x 9 · ú š§ 4     o\  @ /ô  Ç d ” `  ¦ % 3 `  ¦ à º e ” Ü ¼ 9  6 £ § õ 

° ú   .

∆v n = − K r

ρσT δ ∆T (61)

∆p = (η r + ζ 2 − ρζ 1 )K r

ρσT δ 2 ∆T (62) (62)d ” _  F ‹ c   ñ5 Å q _  ° ú כs  — ¸Ž  H “ : r • ¸% ò % i \    5 g € ª œ_  ° ú כ

`

 ¦ t l  M :ë  H \  · ú š§ 4 “ É r “ : r • ¸ Z  }“ É r  â > # 4  A á ¤ s  ß ¼ t

ë ß – & ñ  © œÄ »^ ‰ 5 Å q • ¸  H Õ ª ì ø Í@ / ‰ & ³ © œ`  ¦    · p . s  Q ô

 Ç \ P  â >  Ø  æ   _  : £ ¤$ í  o \  ¦   ? /  H ¿ ºa   H “ : r • ¸ _

 † < Êà º– Ð" f Å Ò# Qt  9 \ P „  • ¸• ¸, ] j1& h $ í > à º, ] j2& h $ í

>

à º\  _ ” > r ô  Ç .    : r& h Ü ¼– Ð ‘ : r ƒ  ½ ¨\ " f  H Ó  o^ ‰ ó ¡ šµ ¢ §

€ 9

2 £ § \  @ /K  – З : r s  ×  æ כ ¹r  ÷ &  H “ : r • ¸ % ò % i \ " f \ P  â >  Ø

 æ   _  $ í | 9 `  ¦ “ ¦¹ 1 Ïô  Ç   õ  Ÿ í 7 H- – З : r   ¨ 8 Š õ & ñ x 9 – Ð

—

: r- – З : r  © œ  ñ Œ •6   x \  _ ô  Ç ™ èY > > à º[ þ t _  % ò † ¾ ÓÜ ¼– Ð \ P  â

>

 Ø  æ    ¿ ºa  “ : r • ¸ 7 £ x † < Ê\     y Œ ™™ è† < Ê`  ¦ · ú ˜ à º e ”

% 3  .

REFERENCES

[1] I. M. Khalatnikov, An Introduction to the Theory of Superfluidity (Benjamin, New York, 1965), Chap.

13.

[2] A. Yu. Iznankin and L. P. Mezhov-Deglin, Sov.

Phys. JETP 57, 801 (1983).

[3] R. J. Atkins and N. Fox, J. Phys. C: Solid State Phys. 15, 947 (1982).

[4] R. J. Atkins and N. Fox, J. Phys. C: Solid State Phys. 16, 1615 (1983).

[5] R. J. Atkins and N. Fox, J. Phys. C: Solid State Phys. 17, 1191 (1984).

[6] R. J. Atkins and N. Fox, J. Phys. C: Solid State Phys. 20, 1937 (1987).

[7] J. R. Torczynski, Wave Motion 7, 487 (1985).

[8] J. R. Torczynski, Phys. Rev. B 39, 2165 (1989).

[9] C. W. Jun, J. Korean Phys. Soc. 41, 820 (2002).

[10] A. Isihara, C. I. Um, C. W. Jun, W. H. Kahng and S. T. Choh, Phys. Rev. B 37, 7348 (1988).

[11] C. I. Um, C. W. Jun, W. H. Kahng and T. F.

George, Phys. Rev. B 38, 8838 (1988).

[12] C. W. Jun, Sae Mulli 58, 569 (2009).

[13] C. W. Jun, New Phys.: Sae Mulli 61, 779 (2011).

[14] C. I. Um, J. R. Kahng and C. W. Jun, J. Korean Phys. Soc. 32, 747 (1998).

[15] C. I. Um and C. W. Jun, J. Korean Phys. Soc. 29, 814 (1996).

[16] A. Isihara and C. I. Um, Phys. Rev. B 19, 5725 (1979).

[17] M. Bretz, J. G. Dash, D. C. Hickernell, E. D. Mclean

and D. E. Vilches, Phys. Rev. A 8, 1589 (1973).

수치

Fig. 1. Temperature variation of the roton-limited thick- thick-ness of the thermal boundary shock wave.

참조

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