• 검색 결과가 없습니다.

NUMERICAL ANALYSIS FOR THE EFFECT OF BLOOD FLOW RATE AND BIFURCATION ANGLE ON THE LOCATION OF ANTERIOR CIRCULATION ANEURYSM AND THE CHANGE OF BLOOD FLOW CHARACTERISTICS AFTER ANEURYSM FORMATION

N/A
N/A
Protected

Academic year: 2021

Share "NUMERICAL ANALYSIS FOR THE EFFECT OF BLOOD FLOW RATE AND BIFURCATION ANGLE ON THE LOCATION OF ANTERIOR CIRCULATION ANEURYSM AND THE CHANGE OF BLOOD FLOW CHARACTERISTICS AFTER ANEURYSM FORMATION"

Copied!
8
0
0

로드 중.... (전체 텍스트 보기)

전체 글

(1)⦽ǎᱥᔑᮁℕŖ⦺⫭                                                          (26일          목) . 제3발표장. 161. CFD응용 Ⅰ. GGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGG. .

(2).

(3) .      . 

(4)                     

(5)              

(6)   

(7)                   

(8)         

(9)   

(10)       

(11)     

(12)    

(13)                 

(14)   

(15) 

(16)      

(17)            

(18)                             

(19)           

(20)                   

(21)                                        

(22)                                 

(23)          

(24)      

(25) 

(26)  !   

(27)                          

(28)              

(29)  

(30)             "       

(31)         

(32)    

(33)   

(34)   #                

(35)       

(36)               

(37)   

(38)     

(39)       

(40)  

(41)   $.      "   

(42) .   !   .     + !&  & &$. " # ! .    ! !  -,./ 0 0        231     +     241 5 5  748  +     ,61  !       !   7,28. .  .  . %  $ &  ('   !# !)!!*. 2011 전산유체 학술대회-2차 수정.indd 161.  . %9 # + # !   7:8 . 2011-05-23 오전 9:56:47.

(43) #  162 제 3 발 표 장 (26일 목).   ⦽ǎᱥᔑᮁℕŖ⦺⫭. CFD응용 Ⅰ. >+ 4  # ;  !    . 0' $. ;'4 ;', ', ;'2 ;': ': ;'- ';'. '. ;'/ ;'3 '3 ;'=. :63< -/2< /23< :63< -/2< /23< :63< -/2< /23<.  

(44) 

(45)   5  64-63-. 6,-6/-.  $4 !&  ! ?   #  "  @. 6-6 .  ' $   74:8 . 7-8. 74-8 4. 5 &74.8 . 7.8 AA &    A?A &    ?  .  . 7/8 & $ 738.  2. 5&7=8 . ?B;?   B!   ; +  0     $&7468    0 !  A B0B!   &  09.  .   . !.   C 7448   $ 7:8. >+ 4. =. !;'4E;'=. .   74,8. !',E'3 . . !  .  ? $ D7428  . 2011 전산유체 학술대회-2차 수정.indd 162.    5  *  74/8  $ 4   F  0    5   0    >+ 4. 0  . ,=.  4=.  ,-. :63<. 2011-05-23 오전 9:56:47.

(46) ⦽ǎᱥᔑᮁℕŖ⦺⫭                                                          (26일          목) . 제3발표장. 163. CFD응용 Ⅰ. GGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGG.  $2 D  @ !  D # .  $, ?  0%! > -/2< /23<. ' :3-. . .  #  '&     . *  74/8 -. .  . 0 .  .    ,.2   . . 2':.  . 4..  . 24.   .  ; 0 (5  466  $  %!  G4, AA &    46-,3  -6-=-  46.43:  ,6//=,    $ , 2:.2/3  A ,-1 ,6//=, . !! . 7438. -.     . 2.   !""!  . . !. '.     #  #   $   %  & . '  (-.     

(47)  . 4.        . 

(48)   

(49) 

(50)   . ,. :. ".   #  () *+ ,. . . -.   (- *+ ,. %  ( ,. .   !"  0    $ 2.    . 

(51) . . 2011 전산유체 학술대회-2차 수정.indd 163. &$74-8. . .  B#   ' $    . 2011-05-23 오전 9:56:48.

(52) #  164 제 3 발 표 장 (26일 목).   ⦽ǎᱥᔑᮁℕŖ⦺⫭. CFD응용 Ⅰ.  $- A   +  #     .  $: A   +  # ;  "  @ 5 . . ". 6-6- 6,-6/-74=8 64-63-74-8  . " .  A.   !#. .  C(;> @.2   .   #  !  , . D0B.  , H . ,6 .  ! :. 2011 전산유체 학술대회-2차 수정.indd 164. . 6664 :  ',6?F. 746,68. A.  AI $ A &   . 7,48 4. A. A. .  . ./00   1. 1. 2 3 35 . 4. .. 2011-05-23 오전 9:56:48.

(53) ⦽ǎᱥᔑᮁℕŖ⦺⫭                                                          (26일          목) . 제3발표장. 165. CFD응용 Ⅰ. GGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGG.  $.@ !   + 0 ' #!# & 0' $  $ :  $     0' $. A A .  A. A    0' $ 5 .  A  0' $.  . 5  .  $/@ !   + 0 ' #!# &  

(54) 

(55)  .  A.   A  5  0' $. 0' $ A. 7,,8.   $ .  $ /. A . 0' $  . 2011 전산유체 학술대회-2차 수정.indd 165.    . 74,8 0' $.  0' $  . 0  . 2011-05-23 오전 9:56:48.

(56) #  166 제 3 발 표 장 (26일 목).   ⦽ǎᱥᔑᮁℕŖ⦺⫭. CFD응용 Ⅰ.  $3 B0   +  #  &  0' $   0 .    .  $=B0  + # &  

(57) 

(58)  . 2  53 3  607       2 3 35 < 9 8. := . . 4. /. 1. . . A . 4.  $ 3  $ = . "!  . B0 B0  ! !  #       B0   B0  0' $  . . B0B!   &  09  A 7,28 A.  ! !  F . B0 7,:8. B0.  B0. 7,,8 B0. B0 . ;. 1. . . 6,. 7,.8. . 2011 전산유체 학술대회-2차 수정.indd 166. 2011-05-23 오전 9:56:49.

(59) ⦽ǎᱥᔑᮁℕŖ⦺⫭                                                          (26일          목) . 제3발표장. 167. CFD응용 Ⅰ. G G G G G G G G G G G B0 G G G G G G G G G G G G G G G G G G G G G G G G GG G G G G G G G G G G G G G G G G G G G G G G G G G G G G G G G. . B0  B0 . B0   . ;

(60) ',663'242'664,. . B0  . . 4  $ I 9.  .   B0 . 0' $ B0. . 0' $.     0' $.   . #. J  A     A . B0  0' $    0' $. A. 5  A   5   0' $      A B0.  0' $ A    B0 . 0' $. 2011 전산유체 학술대회-2차 수정.indd 167. 748 4=/, &+ A( KD&  $ # & ! +  +  IK $ %

(61)   ' 

(62) &  ( '   %%2-4':/6 7,8 4==/ !& I * A0 K0 !     K ) *   + ' @ 22. %%,3':6 728 ,666   0 K $   $ $  !$ F  #  !     K $  

(63)    ,   $     %%42:'423 7:8 4=/,  $  ?? LD& ! #!   &     $ &  %  # &   !   !!    M + )

(64) 

(65)   @ 2/ %%...'.// 7-8 4==4 "  ; L &  !  #  & #   # ! +    M $  @ ,, %%.4='.,- 7.8 ,66: 0$+ $ >   L" # !  $    & % ! # ! +       K + )

(66) 

(67)   @ 464 %%463'442 7/8 ,66/ 5$    L %9 &  !  & %9 #     + # !  ! I!    $  + $ ! +        M $  @ 23 %%4=,:'4=24 738 ,66= & $     L   %  #!   %   &    $       ! +    N  % %   I &  ! 9 & $   !    + ?B;M + - @ :, %%--6'--: 7=8 ,66. 5&    L  !   ! +     +#   #  & #   #    M ' + )

(68)   @ ,/ %%4442'4443 7468 ,646  $& D   L(##! #  * $  &%     &     !   &  9  &   #  !      #  M   )

(69)  )

(70) 

(71)  @ 44, %%26.'242 7448 4=== C  >5  C  ; L I    I     # &  ! !& !  !          M .  ) $ 

(72)  @ ,2 %%422'4:3. 2011-05-23 오전 9:56:49.

(73) #  168 제 3 발 표 장 (26일 목).   ⦽ǎᱥᔑᮁℕŖ⦺⫭. CFD응용 Ⅰ. 74,8 ,663   5   LB & ##! # % '   $  #  %   +    %    >     $ $  !.  *  #  '   &  !M + - @ :4 %%,:4',:3 7428 ,66/ ? $ D   L    % #   .  #  !     M #  + / 0

(74)  0 @ ,3 %%.-2'..: 74:8 ,66-    L %     #  ' $  +   ! !   $   5

(75)  !& OM ,$'* %%,/62',/63 74-8 ,646 &$ (5C   L( +   P!  & $&  %& ! % ! # & P  ! +    M $  @ :4 %%.:/'.-, 74.8 ,66: 5 & >   L4  2  #  ' $ ! + I!  # M .      12 .

(76)  #          #*** *'-$ $  0     %%/,.'/,= 74/8 ,66. *      L & !  ! #    # &   !      + # ! M  )

(77)   @ 4:3 %%42='4:2 7438 4=3- &  0   L(9%  I $  # + !& #    $ 

(78)    +  ##!  & %    #  #      + !& M + - @ 462 %%46,'44- 74=8 ,66. >*    L

(79)  & % + I    & ! ! # A    #      !   . 2011 전산유체 학술대회-2차 수정.indd 168. 7,68. 7,48. 7,,8. 7,28. 7,:8. 7,-8. +        +  # $ !  !. $ $  &      $  

(80) # !  #  46- && I  M  + )

(81)   @ ,/ %%4//6'4//- 4==, ? FF    L0 !          # &  $   % $  M  + )

(82)   @ 42 %%434'433 ,646  $& Q   L &  $ & %   &     %    #  & %  !  # %O  !  % '%! # ! ! %    &  $& !     M       @ ,44 %%::-':-6 ,66- +  Q

(83)    L & ! F  # ! +     #   $ * # %  +  $ % '%! # ! ! %  &  ! M  + )

(84)   @ ,. %%,--6 ,--= 4=3-  ;   LD  #   & !    & &  !   + # ! R D   I !   + %O  !     !  $ &   M        (  - @ - %%,=2'26, 4==.  H   ; LD  #   & &  # !      + # !  I $ !   M 5( + - *  @ 443 %%/:'3, ,662 ?  D   L

(85) % ! +    # $ !  ! $'+ ! %  #   ! %  !  # !   + # !  # M .  - *  @ 24 %%4:, 4-4. 2011-05-23 오전 9:56:50.

(86)

참조

관련 문서

 The rate of change of energy is equal to the sum of the rate of heat addition to and the rate of work done on a fluid particle..  First

1 John Owen, Justification by Faith Alone, in The Works of John Owen, ed. John Bolt, trans. Scott Clark, &#34;Do This and Live: Christ's Active Obedience as the

Bactericidal effect of photocatalytic reactor depending on the UV-A illumination time and flow rate of V.. Bactericidal effect of photocatalytic reactor

The purpose and necessity of this study was to investigate the effect of the 8-week GX complex exercise program on the stress index, blood lipid and APG

 management of the flow of information, products, and services across management of the flow of information, products, and services across a network of customers,

With these results, we can suggest the hypothesis that increased cardiac output in the patients who administered ketamine increased muscle blood flow, and this is the

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

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