䝋䝙䝑䜽䝤䞊䝮᥎⟬䛾䛯䜑䛾㧗⢭ᗘ㏆ഐሙᅽ ຊἼᙧ᥎⟬ᢏ⾡䛻㛵䛩䜛◊✲䠄䛭䛾䠎䠅
◊✲┠ⓗ
ཬ䜃ෆᐜ
ᮏጤク◊✲䛿䠈Ᏹᐂ⯟✵◊✲㛤Ⓨᶵᵓ ⯟✵䝥䝻䜾䝷䝮䜾䝹䞊䝥䛜㐍 䜑䜛㟼⢔㉸㡢㏿ᶵᢏ⾡䛾◊✲㛤Ⓨ䛷ᚲせ䛸䛺䜛䠈䝋䝙䝑䜽䝤䞊䝮᥎⟬ᢏ
⾡䛾䛖䛱Ẽయ㏆ഐሙ䛾ᅽຊἼᙧ䜢㧗⢭ᗘ䛻᥎⟬䛩䜛ᢏ⾡䛾⋓ᚓ䜢┠ⓗ
䛸䛧䠈᱁Ꮚ⣽ศ䛻ᇶ䛵䛟ゎ㐺ྜ᱁Ꮚἲ䛾㛤Ⓨ䜢⾜䛖
ᮾᏛᏛ㝔ᕤᏛ◊✲⛉⯟✵ᏱᐂᕤᏛᑓᨷ
୰ᶫ䞉బ䚻ᮌ◊✲ᐊ
◊✲ᢸᙜ⪅䠖
䕿ᮌ⿱䠄ಟኈᏛ⏕䠅䠈బ䚻ᮌ㍜䠄ຓᩍ䠅䠈୰ᶫ༤䠄ᩍᤵ䠅
Outline
1. ⫼ᬒ䞉┠ⓗ
2. ゎ㐺ྜ⣽ศἲᴫせ
¾
ᩘ್ィ⟬ἲ¾
⣽ศᣦᶆ(Shock Function)¾
⣽ศᡭἲ¾
ゎᯒ3. ᚑ᮶䛾ᡭἲ䛾ၥ㢟Ⅼ䛸ᑐ⟇
¾
ၥ㢟Ⅼ¾
㎶㛗䜢⪃៖䛧䛯䝣䜱䝹䝍䝸䞁䜾¾
ẚ㍑ゎᯒ4. ⤖ゝ䞉ᚋ䛾ㄢ㢟
⫼ᬒ
2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 3
` ㉸㡢㏿᪑ᐈᶵ䛻䛚䛡䜛㦁㡢ၥ㢟
z
ᶵయ䛛䜙Ⓨ⏕䛩䜛䝋䝙䝑䜽䝤䞊䝮䛾పῶ䛜ᚲ㡲z
ᶵయ䛾ప䝤䞊䝮タィ䞉ホ౯䛻䛿䚸ᆅୖ䛷䛾䝋䝙䝑䜽䝤䞊䝮䛾 ṇ☜䛺᥎⟬䛜ᚲせ` ᆅୖ䛷䛾䝋䝙䝑䜽䝤䞊䝮᥎⟬
¾
ఏゎᯒ䛻䜘䜛᥎⟬ἲz
㏆ഐሙ䠖 ᶵయ㏆ഐᅽຊἼᙧz
୰㛫ሙ䠖 䝋䝙䝑䜽䝤䞊䝮䛾ఏz
㐲᪉ሙ䠖 Ẽὶ䛾ᙳ㡪୰ 㛫 ሙ
㏆ഐሙ
୰㛫ሙ
㐲᪉ሙ
⫼ᬒ
` ㏆ഐሙᅽຊἼᙧ᥎⟬䛻䛚䛡䜛せồ
z
ᅽຊἼᙧ⢭ᗘྥୖz
ᐇ⏝ⓗ䛺ィ⟬䝁䝇䝖z
ᐇᶵ」㞧ᙧ≧䜈䛾ᑐᛂ{
ຠ⋡䛾Ⰻ䛔᱁ᏊⅬ㓄⨨䛾ᚲせᛶ{
㉸㡢㏿ᇦ䛷䛿≀⌮㔞䛾ᛴ⃭䛺ኚ䜢䜒䛯䜙䛩⾪ᧁἼ䛜ᨭ㓄ⓗ¾
㠀ᵓ㐀᱁Ꮚ䛻䜘䜛⾪ᧁἼ㡿ᇦ䜢୰ᚰ䛸䛧䛯ゎ㐺ྜ⣽ศἲ
┠ⓗ
` 㠀ᵓ㐀᱁Ꮚゎ㐺ྜ᱁Ꮚ⣽ศἲ䛻䜘䜛
㏆ഐሙᅽຊἼᙧ䛾㧗⢭ᗘ᥎⟬ᡭἲ䛾㛤Ⓨ
z
⾪ᧁἼྠᐃ䛻㛗䛡䛯ᣦᶆ䛸䛧䛶Shock Function䛾ᑟධz
୕ḟඖⓗ䛻⾪ᧁἼ䜢ᤊ䛘䛯㝿䛾ᅽຊἼᙧ䜈䛾ᙳ㡪䛾᳨ド2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 5
NEXST1 ԥ P
ྍどᅗ(ᑐ⛠㠃,R =3)
ึᮇ᱁Ꮚ
⣽ศ(Zӌ0.5) ⣽ศ(Zӌ6.0)
ᩘ್ィ⟬ἲ
` TAS-code (Tohoku university Aerodynamic Simulation code)
`
୕ḟඖ㠀ᵓ㐀ὶయ䝋䝹䝞䞊ᨭ㓄᪉⛬ᘧ ୕ḟඖEuler᪉⛬ᘧ
✵㛫㞳ᩓἲ 䝉䝹⠇Ⅼ᭷㝈య✚ἲ
ὶ᮰ホ౯
HLLEWἲ
㛫✚ศ
LU-SGS㝜ゎἲ
! 1
shock
f f shock 1
⣽ศᣦᶆ(Shock Function)
2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 7
` ⾪ᧁἼྠᐃ䛻㛗䛡䛯Shock Function䛾ᑟධ
z
⾪ᧁἼ㠃㏆䛻䛚䛔䛶Ἴ㠃䛻ᑐ䛧ᆶ┤䛺㏿ᗘᡂศV
n
䛜㡢㏿䜢䜎䛯䛠ᛶ㉁䜢⏝a M V
f
p V p
V
n n shock
n
x &
&
&
ᅽຊ໙㓄࣋ࢡࢺࣝ
㡢㏿
㏿ᗘ࣋ࢡࢺࣝ
: :
:
p a V
&
&
p &
V &
) Shock
( p & A
V & n
Shock ) 1 ( f shock
⩼㠃ୖ䛾⾪ᧁἼ㡿ᇦྍどᅗ
(M=0.84䠈f shock =1➼್㠃)
㉸㡢㏿ᇦୗ䛷䛾ᩘ್ㄗᕪ䛾ᙳ㡪
` ㉸㡢㏿ᇦ䛷䛿ᩘ್ㄗᕪ䛜⾪ᧁἼ㠃䛾ྠᐃ䛻ᙳ㡪
z f shock
䛾䜏䛷䛾ྠᐃ䛜ᅔ㞴` ᅽຊ໙㓄䝣䜱䝹䝍䞊䛾ᑟධ
¾
ᅽຊ໙㓄䛜㜈್䜘䜚䛝䛔㡿ᇦ䛷ุᐃ䜢⾜䛔,ᩘ್ㄗᕪ䜢㝖ཤE thr
p t
&
E thr :䝣䜱䝹䝍䞊㜈್(ᐃᩘ)
䝣䜱䝹䝍䝸䞁䜾䛺䛧 䝣䜱䝹䝍䝸䞁䜾䛒䜚(E
thr =0.01)
f shock
䛾ྍどᅗ(M=1.41, ᑐ⛠㠃)⣽ศᡭἲ
` Bisection䜰䝹䝂䝸䝈䝮䛻䜘䜛ศ
`
ᅄ㠃య䛾᭱㛗㎶䛾୰Ⅼ䛷ศ` ィ⟬䛾᮰ᛶ䛾ᨵၿ
`
⣽ศᚋ䛾᱁Ꮚ䛻䚸⣽ศ๓䛾≀⌮㔞䜢ෆᤄ
2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 9 Shock Function 䛻䜘䜛
⣽ศุᐃ䛸⣽ศ䛾ᐇ⾜
⣽ศᚋ䛾᱁Ꮚ䛻
⣽ศ๓䛾≀⌮㔞䜢ෆᤄ
ᗘ䚸ᐃᖖゎ䛾ゎᯒ ᱁ᏊⅬᩘ䛾ቑຍ䛜䛒䜛䛛
ึᮇ᱁Ꮚ䛻䛶 ᐃᖖゎ䛾ゎᯒ
⤊
Yes
No
h/L=5.0 h/L=3.0
ԥpศᕸ(ᑐ⛠㠃)
h/L=5.0 h/L=3.0
ึᮇ᱁Ꮚ(ᑐ⛠㠃)
` ゎᯒᑐ㇟
z ㍈ᑐ⛠≀య
z A(x)=0.02x (0ӌxӌl)
z
䡈䠙2in.
` ゎᯒ᮲௳
` ึᮇ᱁ᏊⅬᩘ䠖⣙55Ⅼ
` 䝬䝑䝝ᩘ 䠖1.41
` ㏄ゅ 䠖0㼻
` ᅽຊἼᙧྲྀᚓ⨨
z ᑐ⛠㠃ୖ
z h/L=3.0䠈5.0 (ᐇ㦂್)
ゎᯒᑐ㇟䛸ゎᯒ᮲௳
L=1 3L (䝇䝔䜱䞁䜾㒊䜢ᶍᨃ)
` Shock Function
z ᅽຊ໙㓄᪉ྥ䛾㏿ᗘᡂศ䜢⏝䛔䜛䛯䜑
್䛜Ᏻᐃ
` ᅽຊ໙㓄䛾⤯ᑐ್
z ῶ⾶䛾ᙳ㡪䛻䜘䜚,㐲᪉䛷䛿ኚື㔞䛜ῶᑡ
h/L=0.5 h/L=1.0
ᣦᶆ䛾ឤᗘẚ㍑
2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 11
ึᮇ᱁Ꮚ䛻䛚䛡䜛ԥpศᕸ (ᑐ⛠㠃)
0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2
-1.5 -1 -0.5 0 0.5 1 1.5
0 1 2 3
P res su re G ra d ie n t[- ]
S h oc k F u n ct io n [- ]
x h/L=0.5
ShockFunc PressureGrad
0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2
-1.5 -1 -0.5 0 0.5 1 1.5
0 1 2 3
P res su re G rad ie n t[ -]
Sho ck F unc ti on [- ]
x h/L=1.0
ShockFunc PressureGrad
ĺᗈ⠊ᅖ䛷䛾ุᐃ䛷䛿䠈Shock Function䛜᭷ຠ
Case1 Case2
Case3 Case4
⣽ศ㡿ᇦཬ䜃᮲௳
` ┤᪉య䛾⣽ศ㡿ᇦ
` ⣽ศᑐ㇟䛾ุᐃ
z
⣽ศ㡿ᇦෆz
ᅄ㠃య䛾᭱㛗㎶䠚ศ㝈ᗘz
௨ୖ䜢‶䛯䛩ᅄ㠃య
Case1 Case2 Case3 Case4
ᅽຊ໙㓄䝣䜱䝹䝍䞊
⣽ศ㜈್
ศ㝈ᗘ
0䍺z䍺0.1 0䍺z䍺0.5 0䍺z䍺1.0 0䍺z 䍺2.0
⣽ศ㡿ᇦ
E thr =0.01
|f shock |䍻1(⭾ᙇ㡿ᇦ䜢⪃៖)
0.05 0䍺x 䍺10 -6䍺y䍺0
t 1
t
p & E thr f shock
⤖ᯝ(᱁Ꮚ)
2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 13
Case1(0ӌzӌ0.1) Case4(0ӌzӌ2.0)
ึᮇ᱁Ꮚ
ึᮇ᱁Ꮚ Case1 Case2 Case3 Case4
⣽ศ䞉ィ⟬ᅇᩘ - 12 13 15 18
᱁ᏊⅬᩘ ⣙㻡㻡Ⅼ ⣙㻡㻤Ⅼ ⣙㻣㻡Ⅼ ⣙㻥㻠Ⅼ ⣙㻝㻟㻜Ⅼ
⣽ศ㡿ᇦ ⊃䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷䚷ᗈ
Case2(0ӌzӌ0.5) Case3(0ӌzӌ1.0)
ᑐ㇟㠃ཬ䜃x-z᩿㠃(h/L=5)Case1 Case2
Case3 Case4
⣽ศ㡿ᇦ
⤖ᯝ(ԥpศᕸ)
Case1(0ӌzӌ0.1) Case4(0ӌzӌ2.0)
ึᮇ᱁Ꮚ
Case2(0ӌzӌ0.5) Case3(0ӌzӌ1.0)
` Case1
䠖ᅽຊኚື䛜ῶ⾶` Case2
䠖᭱䜒䛝䛺ᅽຊኚື` Case3,4䠖ศᕸ䛜Ᏻᐃ
ᑐ㇟㠃ཬ䜃x-z᩿㠃(h/L=5)
Case1 Case2
Case3 Case4
⣽ศ㡿ᇦ
` ⣽ศ㡿ᇦ(z㍈᪉ྥ)䛻䜘䜚Ἴᙧ䛜ኚ
z h/L=3䠖Case3(0ӌzӌ1.0)
䛷᮰z Z=0.5䛾䛸䛝ึᮇᅽຊୖ᪼䛜᭱䛻
z h/L=5䠖ᮍ᮰
⤖ᯝ(ᅽຊἼᙧ)
2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 15
-0.02 -0.01 0 0.01 0.02 0.03
-1.5 -1 -0.5 0 0.5 1
h/L=3.0
nona dp Ca se1(z0.1) Ca se2(z0.5) Ca se3(z1.0) Ca se4(z2.0)
4 3
¸ ¹
¨ ·
© ' §
L h p
p
4 1
¸ ¹
¨ ·
© ' §
L h L
x
-0.02 -0.01 0 0.01 0.02 0.03
-1.5 -1 -0.5 0 0.5 1
h/L=5.0
nona dp Ca se1(z0.1) Ca se2(z0.5) Ca se3(z1.0) Ca se4(z2.0) Exp
4 3
¸ ¹
¨ ·
© ' §
L h p
p
4 1
¸ ¹
¨ ·
© ' §
L h L
x
h/L=5.0 h/L=3.0
Ἴᙧྲྀᚓ⨨
⤖ᯝ(⣽ศ㡿ᇦ䛾ᅽຊศᕸ䜈䛾ᙳ㡪2)
x-z᩿㠃(h/L=3)䛷䛾ԥpศᕸ
Case2(0ӌzӌ0.5) Case3(0ӌzӌ1.0)
Case4(0ӌzӌ2.0)
` ᅽຊἼᙧ䜢ྲྀᚓ䛩䜛㝿䠈㡿ᇦ➃㒊䛾ᙳ㡪䜢⪃៖䛩䜛ᚲせᛶ
⣽ศ㡿ᇦ
⣽ศ㡿ᇦ
⣽ศ㡿ᇦ
ᚑ᮶䛾ᮏᡭἲ䛻䛚䛡䜛ၥ㢟Ⅼ
2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 17
z タᐃ䛧䛯᭱ᑠ᱁Ꮚ䝃䜲䝈(ศ㝈ᗘ䠖5e-2) 䛷䛿Ἴᙧ䛜ῶ⾶
z Z㍈᪉ྥ(䝇䝟䞁᪉ྥ)䛾⣽ศ㡿ᇦ䛻䜘䜚,
ྲྀᚓ䛥䜜䜛ᅽຊἼᙧ䛜ኚ
¾
䜘䜚⣽䛛䛺⣽ศ(ศ㝈ᗘ䛾⦰ᑠ)¾
⣽ศ㡿ᇦ䛾ᣑᙇ(㡿ᇦ䛾ᙳ㡪䛾᳨ド)ڹ ᱁ᏊⅬ䛾ቑຍ䛻䜘䜚,ᚑ᮶䛾䜎䜎䛷䛿ィ⟬䝁䝇䝖䛜㠀⌧ᐇⓗ
z
⣽ศ㡿ᇦ䜢᭱ᑠ䝃䜲䝈䜎䛷⣽ศ䛩䜛䛯䜑,᱁ᏊⅬቑຍ䛜ⴭ䛧䛔z
ศ㝈ᗘ䜢⾲㠃᱁Ꮚ䝃䜲䝈(1e-2௨ୗ)䛻䛩䜛䛸,䝰䝕䝹㏆ഐ䛾ᩘ್ㄗᕪ 䛾ᙳ㡪䜢ཷ䛡䜛ุᐃ䛾ᨵၿ䛜ᚲせ
᱁ᏊⅬᩘቑຍ䛻┤⤖
ᅽຊ໙㓄䛻䜘䜛䝣䜱䝹䝍䝸䞁䜾
` ᚑ᮶
`
⠇Ⅼᇶ‽䛷䛾ุᐃ(ྛ⠇Ⅼ䛾ᅽຊ໙㓄䛾䛝䛥)`
㜈್䜢ᡭື䛷ධຊ䠈ྛ⠇Ⅼ䛾್䛜㜈್䜢ୗᅇ䜛ሙྜ䛻㡿ᇦุᐃ䛛䜙㝖እ
` ᪂䛧䛔ᣦᶆ
`
㎶ᇶ‽䛷䛾ุᐃ` (ྛ㎶䛻᥋䛩䜛⠇Ⅼ䛾ᅽຊ໙㓄್䠈edge䛾㛗䛥)
`
ධຊ䛥䜜䛯≀⌮㔞䛛䜙㜈್䜢タᐃ`
ᚲせ䛻ᛂ䛨䛶㔜䜏䛡䜢᳨ウedge L edge
p
f x |ѭp| edge䛻2⠇Ⅼ䛾ᖹᆒ್
|ѭp| edge , L edge
䛻㔜䜏䛡↓䛧䝣䜱䝹䝍㜈್䛾タᐃ
0 50000 100000 150000 200000 250000 300000
1.0E-10 1.0E-08 1.0E-06 1.0E-04 1.0E-02 1.0E+00
ed g e ᩘ
|ѭp|*Edge_length
䝣䜱䝹䝍ᣦᶆศᕸ䝣䜱䝹䝍ᣦᶆ䛾ศᕸ䛷᭱ᩘ䜢䜒䛴್䜢㜈್䛸䛧 㜈್௨ୖ䛾㡿ᇦ䜢ุᐃ㡿ᇦ䛻タᐃ
|ѭp|
㎶䛾㛗䛥
3.3E-4 0 0
50000 50000 100000 100000 150000 150000 200000 200000 250000 250000 300000
⣽ศุᐃ
2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 19
䝣䜱䝹䝍䛾ẚ㍑(PGF 1e-2 , edge)
ྛ⠇Ⅼ䛤䛸䠈E
thr =1.e-2
ྛ㎶䛤䛸䠈(¶thr = 3.3e-4
9᱁Ꮚ䛜⣽䛛䛔䜋䛹䝣䜱䝹䝍䛜ᙉ䛟ാ䛟
¾᱁Ꮚ䝃䜲䝈䛻ᛂ䛨䛯䝣䜱䝹䝍䝸䞁䜾
ᙉ
ᙅ 䝣䜱䝹䝍ᙉ䛥
᱁ᏊⅬᩘ: 130Ⅼ
PGF䠖 1.e-2(node)
ศ㝈ᗘ䠖5e.-2
⣽ศᅇᩘ䠖18
᱁ᏊⅬᩘ䠖 䠔䠒Ⅼ
PGF: edge
ศ㝈ᗘ䠖
5e.-2
⣽ศᅇᩘ䠖7
᱁ᏊⅬᩘ: 170Ⅼ
PGF: edge
ศ㝈ᗘ䠖
1e.-2
⣽ศᅇᩘ䠖10
᱁Ꮚẚ㍑
` 䝣䜱䝹䝍䛻㎶㛗䜢⪃៖䛩䜛䛣䛸䛷,ᅽຊ໙㓄䞉㎶㛗䛻ᛂ䛨䛯⣽ศ
䛜ྍ⬟䛻
䕿䜘䜚⣽䛛䛺⣽ศ䛜ྍ⬟
(䜘䜚⣽䛛䛺ศ㝈ᗘ)
䕧㐲᪉䛾໙㓄䛜ᑠ䛥䛔㒊ศ䛷,༑ศ䛺⣽ศ䛜㞴䛧䛔2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 21
h/L=1.0
`
⠇Ⅼᇶ‽䛾䝣䜱䝹䝍䕿㐲᪉䛾⣽ศ䛻᭷ຠ
䕧ศ㝈ᗘ䜢⣽䛟䛷䛝䛺䛔
`
㎶ᇶ‽䛾䝣䜱䝹䝍䕿ศ㝈ᗘ䜢䜘䜚⣽䛟䛷䛝䜛
䕿䝰䝕䝹㏆ഐ䛾ᩘ್ㄗᕪ䜢㝖ཤྍ⬟
䕧㐲᪉䛾⣽ศ䛷༑ศ䛺⣽ศ䛜ᚓ 䜙䜜䛺䛔
ᅽຊ໙㓄䛾ẚ㍑
-0.02 -0.01 0 0.01 0.02 0.03
-1 -0.5 0 0.5 1
h=3
PGF_1e-2 div5e-2 PGF_edge div5e-2 PGF_edge div1e-2
-0.02 -0.01 0 0.01 0.02 0.03
-1.5 -1 -0.5 0 0.5 1
h/L=1
PGF_e-2 div_5e-2 PGF_edge div_5e-2 PGF_edge div_1e-2
-0.02 -0.01 0 0.01 0.02 0.03
-1 -0.5 0 0.5 1
h/L=5
Exp
PGF_1e-2 div5e-2
PGF_edge div5e-2
PGF_edge div1e-2
䝣䜱䝹䝍㜈್䛾ኚ
2010/11/26 Yusuke OKI, Dept. of Aerospace Engineering, Tohoku Univ. JAPAN 23
`
⣽ศ䛻䜘䜛⤖ᯝ䛾ᨵၿ䛻䜘䜚,䝣䜱䝹䝍䛾㜈್䛜䛝䛟䛺䜛(䝣䜱䝹䝍䛜ᙉ䛟䛺䜛᪉ྥ䜈䝅䝣䝖)
䕿䜘䜚⣽䛛䛺⣽ศ䛻᭷ຠ䕧㐲᪉䛷䛿䝣䜱䝹䝍䛜ᙉ䛩䛞,⣽ศ䛜༑ศ䛻
ᣦᶆ䛾㔜䜏䛡,㜈್䛾Ỵᐃἲ䛾ᨵၿ0 200000 400000 600000 800000 1000000 1200000
1.0E-10 1.0E-08 1.0E-06 1.0E-04 1.0E-02 1.0E+00
ed g e ᩘ
|ѭp|*Edge_length
䝣䜱䝹䝍ᣦᶆศᕸ⣽ศ๓
⣽ศᚋ
3.3E-4 2.2E-3
⤖ゝ䞉ᚋ䛾ㄢ㢟
` ⤖ゝ
ż
ᩘ್ㄗᕪ㝖ཤ䛾䛯䜑䛻䠈ᅽຊ໙㓄䞉㎶㛗䜢ᣦᶆ䛸䛩䜛䝣䜱䝹䝍䜢ᑟධ䛧䠈ᣦ ᶆ䛾ศᕸᩘ䛛䜙䝣䜱䝹䝍㜈್䜢⮬ື䛷ồ䜑䜛䜘䛖ኚ᭦䜢ຍ䛘䛯ż
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