다.5 Dimental Analysis and similan.ly
I Planning , pantatm.mterpetatmofexplCFD.ua
9, µ
ㅇ缸
→ F. ⇒ F - f ( t.V.9.pe )FI_i.fi#' at
쏌
Least 10 datap.imstt0 "
(God V. 9. µ) (E points for b each L. V.
f.M.BAA wereda are Nation to
唜一 이땄
) ←弑潞
OEEdimeansmod
analysis ,
〖%faae-stoexpsaiy.l.EE
RefRm.ae = RMtotype → G mode = G.pro
totpe.no/rmfelllf.Er5.2.Pmcrpleofdmensmalhomogenei
ty .→ in te same of , each adaHe term should
have are same dina위다.
( ftftv.ttgo.tlIst[ ㄴ] Cha Falling)
1 ¥ .it gz = constant (Bernardi q)
/ ' iii] S
⇒ dimental variable : S. V. t.pe z . .
( a constant : So , 당 , g, . . .
- Pure constants →
nodimensia.eguatiin_dmsiadeeseguiuo.intanalysis
non_dimental form
5.3 .
[email protected]ion in variable
( n : diMenand variable
( k : " loss variable ( TI )
↳
reactionj = n - k < number of
dimensrousnecessangtodescribed.imemotional variable
延
정 atitaf.E.TL?reductrmj=5-=f
a' cnv.em.netk£ 3 ∴ k 32 .G. . g ( Re ).fr?T=G.Tz=Re
② Find The reaction
Ni = fwz.rs. 다.V5 ) 7=5
if 3 diMasters [ M.LT 〕 arevequired.kz?
⇒ T.wsask.US. 이 .me i]
gdimen.si예의s
E = www.iwaf V5 = LM인0T에 1
☆ I
form Pi Group by Power Product of
these variable that to not form a Pi
↳
(mi mi Nd = cnet.my 세대receptor
a= b =C = 0
diMensuit analysis oilI tail .
:
F:
=:
f:
( L . v:
. 9:
):
T-T:
✗:
-choosedensity.ve/ocityadIengjodonotputturodependentvariable as
reaction variable
.
ex) E = ftp.L.U.ru ). N- 5 .
F = [ MLFT
/
대.LT 〕 5k£ 3L - 다]
8.32.0 4 kt 2.
V2 CLI' 〕
t.fi[ ME3] j variableS .
µ .fm 幽巧 L
. V . 9 .
( ftp.CNET?a.b.C? )
T.tt CE = (LIKE 'J 〔 M I[ MLE정
= [ int53
에
f"? M에
〕 = [ ☐ TN 〕→ a-2.be -2, C = - 1 .
i. T-T V29" F =
唜泄
G)石一一 ☐ ftp.fmiija#=C-l_ee.
∴
石二唜 一恨
. ( 또' - '佑二
Re )LG.ge?nedspractiee!fmi3S=fcPcL.E
.IT ""에
豺 .it?.E.&SttnyfMLiI
iii]( j - 5 - k£3 . E32 .
Can'tb And to ㅠ groupS , because P and
E contan M and F but also same Power
of Mad T . ⇒E230
T.ME" S
(
퍄샤탸
P ⇒ E. = 8恁悠
_ . )形二
池邨工
•
뛨
Gene←!) Q #.mn#CMeLcTR.쀲
〕 . 4 - 요 £ 3EarlI Group : T.it#dQ=CM F]
Q = AV d,
퍄 公器八
= constant = cr T
M = HR
惚心
GQ.ci .it (
邨仙
) .- 9 Q .
→ 9 9
54 alon-dimeoodizatmofthebasiceqwtms.in
inwmpressibkflowi.wntmity.FI = 0
( - its equation : 9
慶一加
trea material denrate
ISNon - dimensimdizo.tn 렁 i.
→ characteristietalesneededl.LIU )
,
5. 4. Non- domensrnalizatoan 0f the 트basiiegn
mnompresibleftoror
↓
ontonuity : OOA- 브 = 0
* mtm : aptuO9 -matewalOO- derivative
오
o*we need charaoterstr scale도 .
b velocity , length, …
A ( ω ) CL )
e - q ) 브 =
는
구
*
= -
또
, YA=보
,
E
*
= E ,
A
= P
t * = =
단
. P 9 ω 국- ( 2-=2α((vuLx*← ) = 온 쳐 ⇒ 하 = 1. 보한*
9 - ( = -D9D((t*UI
는
*) ) =9 년…맨
AI
MoOP=== MoEA* ( p**(e어스
) = -← ) 0=양
( JXPd*짜서르서
)**
은
* =
-[90중식 * tM않*
르으
* [ UA서
만
* = -☆*p *청
+남 LO*르*. P =
앓 홉
1
d = -Mertia
Nscousforc②
2
맡*+ (
스
:O *)L *= - Oxp* * + ke* 8A로서
ADomenstonal Parameters
. Re = ~9(압 Reynoldsmomker))
. Fr = CFroude number) ~ shipriver, sea
We= - f람(Webernumber)- interfacialflowr
liqurd droplet .
- surface fenson
Maz 남 ( Machnumber)
st= - 참( strmhalnumherx
오
frequencyO O
요 법
, sensor O이
L Kanman vortex shedding
나스 W . coscft )
.
남
= uA = ws ( ft대는
)= cos ( st. t* ) ,
- pr =
음
uc ( Prandtl namber) [ FU -Athermalconductivity g = - k -
업
다 =
불며
0) G = -ieurAOndrag,1 Lift ( (항력 ) .
lift (양력) drag coeffrcieut
wefftcient
- → O…~…
8w C " §
P = P
- P
일
e 며( pressure oefficiewA))
5.5 . Mo .delingandSimplantyy ( 상사성)
ππ= f(π iπ 3 … )
5π 2m= π p, π 3m=π zp, … ⇒π im = πiP ,
* GeometreEimilavity [ L ]
a mmodel and Protofype ane gmetically similan
ifand onlyif all body dimensins in all three
coordinateshaethesamelMear -sealerato :
> all angles are presened, all flow directronsane
preservedd
co~ -00…EX
* ㅡKinemafic 9imflarty [ L . T ]
themofionsofftwo systems ane Simiplar→
model ndfprofotype hal tle same
C
length- and fime - scale
ratocC
-+AP 나(속도)
AM
사1 CM
~Hp
Perod: Tp ②
남
~4m Tm m→Froude number , 2
Fvm =
했다
ㅋ 됐=-. -5
하
Dt ② : vm = VD ⇒ Vm = rav
Tm = raTr
y [ TJm, 다 .
namme* similaity
- Same lenyth - , fime - , and mass (force)
-scale rattos,
동 P ∞
> ㅋm
; Am, 9 m O
남 . 9p " 섬
∞ m
Renp OL'=-fpvoplup,Rem =-µn/=σm
[ f dm = adp, same fluid, 참 m =
호
APRealㅡflows ~> lab tests . CCED , EXP)
ㅡ *
nwmpressibe flow . Reㅡ
( compressibe flow : Re & ㅡㅡMas