• 검색 결과가 없습니다.

Unsteady Aerodynamic Analysis of Helicopter Rotor Blades Using Diagonal Implicit Harmonic Balance Method

N/A
N/A
Protected

Academic year: 2021

Share "Unsteady Aerodynamic Analysis of Helicopter Rotor Blades Using Diagonal Implicit Harmonic Balance Method"

Copied!
7
0
0

로드 중.... (전체 텍스트 보기)

전체 글

(1)⦽ǎᱥᔑᮁℕŖ⦺⫭                                                          (27일          금) . 제3발표장. 543. CFD응용 Ⅶ. 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)   

(43)   

(44) $ 

(45)  

(46)  

(47) %

(48) 

(49)       . . ).*. 

(50) . )/$0*. %( - ("& +" . 1" . )2*. .  &&. ) *. .   +(+#&&. )$*.

(51) 34  , " . . )* . - ("& +"   . !.

(52) !  #"  %$& ! '#(. 2011 전산유체 학술대회-2차 수정.indd 543. 2011-05-23 오전 10:06:55.

(53) #  544 제 3 발 표 장 (27일 금).   ⦽ǎᱥᔑᮁℕŖ⦺⫭. CFD응용 Ⅶ. ! .

(54) 34. . )8$ * .  . .            . . 5 6.  . .

(55). . . !. . . .           5 6.  .  .   

(56) 

(57)      

(58) . 56. 

(59) 

(60)     

(61) . .  . . . . 56.

(62)     %  #$. ". ). '. (. . . F . ". G "

(63) . . . . 5 76.         

(64)      .  . "  #$

(65) . . 586. .                 . . . .           

(66)         . 

(67)    .   . 586. 56. . 56. 526  5 76. . . .   . 5.6.   . 5/6.  . . . .   . .

(68)        

(69)          . 506.  .  !"#$%)((#'&*+ -.,/01274365*8:;.9=< +?>5@*A*BDCE8       

(70)      . 5 6. 5 6. . &   ' .

(71)       .              .                      . .    .         

(72)         . . 5 6. . 526. . 2011 전산유체 학술대회-2차 수정.indd 544. 2011-05-23 오전 10:06:55.

(73) ⦽ǎᱥᔑᮁℕŖ⦺⫭                                                          (27일          금) . 제3발표장. 545. CFD응용 Ⅶ. GGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGG . . . !!     ).* 5 6. .   . # #.      

(74)            . 3# ,5

(75) 9-#?!"@&  A.0A 6. 5 6. # #.             

(76)     . 5 6. 56 5. A.0A  2= /. (6. .  

(77) . . #$"%. . .  (&&("B "( . 78. . . ) * . !". . !" . .

(78)  9 -#. . ) *. . ;:

(79) :77  0.<"5  6 2= .  78. / 7200. . 2011 전산유체 학술대회-2차 수정.indd 545. .  -@&  - #!"

(80) <<(" 5+C786.   . . *%. +#&"$>&(. 2011-05-23 오전 10:06:56.

(81) #  546 제 3 발 표 장 (27일 금).   ⦽ǎᱥᔑᮁℕŖ⦺⫭. CFD응용 Ⅶ. 3# 

(82) B( < & < !"D.  EF C 7.. @ EF C 7/2. ( EF C 727.  EF C 728. EFC78/ 3#  !!#

(83) <<(" !"@#"  >& #<( 5 +C78 6 . #'&&. 7200 . 3# 

(84) B( < - #!"

(85) <<(". 2=. . 7.  7/2  72  728  78/ . .  . . . .. 7/2  727  728  78/. . .  . 2011 전산유체 학술대회-2차 수정.indd 546. 2011-05-23 오전 10:06:56.

(86) ⦽ǎᱥᔑᮁℕŖ⦺⫭                                                          (27일          금) . 제3발표장. 547. CFD응용 Ⅶ. 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 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  2  H.  @ -@&  - #!"

(87) <<(" 5+C72006.  ( 8 *% .  . 2. . .. .  EF C 7/2. @ EF C 727. 3# /

(88) B( < & < !"D 5;$&<" 3 3& "6. ( EF C 728 EFC78/ 3# . !!#

(89) <<(" !"@#"  >& #<( 5 +C7200 6  !"!

(90)  9 -# "( 3&. )  8* (&&("B "(   0  -  +( .  7. 7. +  ,-. +  .-. +  /-. +  -. 72 .  /.   . . 0. 28G. 8. 2011 전산유체 학술대회-2차 수정.indd 547. 2011-05-23 오전 10:06:59.

(91) #  548 제 3 발 표 장 (27일 금).   ⦽ǎᱥᔑᮁℕŖ⦺⫭. CFD응용 Ⅶ.   . . +  0+  13# 0 !!#

(92) <<(" !"@#"  >& #<( 5 EFC728  ;$&<" 3 3& " 6. . . 7 . . 5. 6 5;. 7 $777206   (. @  (!. (  (! 3# 2 #<( !!#

(93) "#!  <<" (! 5;$4<" 3 3& "6 -@&  ;$!& - " <<" (! 5;$&<" 3 3& "6. ". 2011 전산유체 학술대회-2차 수정.indd 548. ) * 77  &&  

(94)   - !   

(95) &  I   J

(96)  #"" < K!"D ;& 3&! 

(97) !(! K!  ( >&( -( L# J &&& '     M&7  ;.  208$22/ )* 77  +(+#&&  +  !  :  :&!    J: &(" <  ;$4 3L#(D  &B " "  %#&  ;B$ "! %L#"! J )(  &&& &

(98)  

(99)  *

(100) 

(101)  +

(102)

(103)   ,%  )* 77/  +(+#&&  +  !  :  :&!    J!"" < ;& 3L#(D  +" ! J &&& '   M&  ;0   2$ . )* 77.  , "  :  !  :  J- ("&+"  < ( K!"D

(104)  #""! B -$  - $!& >! J )- &&& &

(105)  

(106)  *

(107) 

(108)  +

(109)

(110)   ,%  ).* 772  %(    &&  

(111)   &&  %  J

(112)  #""&&D 3!" ( >&( +" ! < K!"D :D( ("! < &( " F"! J #& <

(113)  #""&  D!(!  M&0  /7/$/. )/* 772 

(114)      ""  :  N

(115) 3 (" < F" 4! K! -$ ("& +"   %O(" 3&#$ "#("# "<(N  /"  ::: : & :D(!. 2011-05-23 오전 10:07:02.

(116) ⦽ǎᱥᔑᮁℕŖ⦺⫭                                                          (27일          금) . 제3발표장. 549. CFD응용 Ⅶ. G G G G

(117) <(  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 G G G G G G G G G G G G G G G G 

(118)   G G G G G JK!"D G G G G G G G G3& G G G G

(119)  #"" K!  ( )0* 772 

(120)     "!  +  4    ((  ,   :&!     N&( " F" ! K!  -$ ("&  :1"$>! +" N  "  :::E +P +#&"!( &D :&D!!  P "Q"

(121) <(  >"! 

(122) &#@ 

(123) . . .  R )2* 7 7 . N .    0/$2 )8* 778  I"  +:  >((    J &(" ( >&( &B < -!( 3& "  3( +"! J &&& '   M&0  ;  28$87  ) 7* 778 

(124)      ;1    J &(" ;& 3L#(D$ ("&$<<( (  < ( %#& 3& J &&& '   M&0  ;  / $0 ) * 778  - !    

(125) #!" 

(126)    &&  %  && . 2011 전산유체 학술대회-2차 수정.indd 549. >&( : (   &" @#" "  PM%F34PI  3& &B J ./  &&&      0  

(127) 

(128) 

(129)  ) * 77      J (" +" ! < D( "@&"D B"B! K! "  ;B$ "! %L#"! N   !!""   " < :! ( %  : -  1   ) * 82 

(130)   3S  -# 

(131)   J%O "&  :&D"(& "#! <  +& &( " F"  B J ;: : -+$2  ) * 77        T       J(" <  

(132) <<("! K! "  K!"D %#& %L#"! J '   * 

(133)     12

(134)   M&7  ;   ./$/. 2011-05-23 오전 10:07:02.

(135)

참조

관련 문서

9 Designed aerodynamic shape of 500W class wind

Aerodynamic noise noise noise that noise that that that happen happen happen happen in in in in unsteady unsteady unsteady flow unsteady flow flow flow of

period was prolonged unavoidably, (3) by explaining the risk factors associated with the failure to patients honestly, and subsequently performing

Currently, the method of radioactive strontium( 90 Sr) analysis uses the nitric acid method and resin method.. The act of nitric acid method and

Global structural analysis model of the 300K VLCC by using the developed method. (Shell element, 1-D

The advent of flap hinge (Renard - 1904) relieved the blade root moment, by allowing the blades to flap freely in response to oscillatory aerodynamic flap moments.. 1.2

The advent of flap hinge (Renard - 1904) relieved the blade root moment, by allowing the blades to flap freely in response to oscillatory aerodynamic flap moments.. 1.2

Reference 7 contains a derivation (also by the Newtonian method) of a system of nonlinear equations for the elastic bending and rigid pitching motion of a cantilever rotor