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Data Kapal :

L (Lpp) = 128 m =

L (Lwl) = 131.84 m

L Disp = 129.91 m g =

B = 22.4 m 1.7 T=

H = 11.3 m k =

T = 7.817 m .!9 " 22.42 =#$ = .!9 m .!9 " 22.42 % 1&7 T =

#p = .7 m

#m = .983 m

's = 19.2 Kt 9.87!48

*a+i,s -la/a0a = 27.821 a,tial ils

-g5it,ga Ta5aa $0+asa0ka mt+ 6,l+5amm0Ha0al+

1. Perhitungan Volume Displacement dan Displacement

= L " B " T " #$ == 131.83 " 22.42 " 7.819 " .!9 =

= 1928.8 =

2. Permukaan Basah Kapal

B0+asa0ka ,m0+ 0m,la

(H;*';LD ..31& T;H;; D; -*? K;-;L& pag 133)

> = 1,025xLpp(Cb x B+1,7T)

= 1.2 " 127.99 " (.!9 " 22.42 % (1.7 " 7.819)

= 3771.339

3. Nilai Froude dan Reynold Numer

= * =

= .2747!7! =

!. "oe#cient Friction $"%& Lg * =

# = Lg * 2 =

= .1134

Ti+ak a+a k0ksi aggta $a+a kapal /ag mlip,ti +a, km,+i& l,as $ilga& $

ka0a p0m,kaa $asa5 aggta $a+a kapal 0lati kil& s5igga +apat +ia$a

'. "oe#cient Resistance $"r&

#0=

= .238442 @1A3 =

'sA(g " Lwl).

.7A(lg*2)2

(Lg * 2)2=

Lwl/1/3

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10 CR it0plasi

1 5 1

2 5.237 0.9289

3 5.5 0.85 (2a1a) =

(3a1a) =

K0ksi ksi ta5aa kapal C(2a1a)A(3a1a) =

a. $t,k $a+a kapal

,t,k mg5it,g ta5aa pa+a $a+a kapal mgg,aka m+l p0$aa Ea+

$. *asi BAT

Ka!"a #$a%a& 'aa"a" '!!b*' #$b*a' b!#aaa" a$ L!ba-aa' B/T = 2,5

&aa apal a"% &!&p*"a$ l!ba-aa' l!b$ b!a a'a* l!b$ !$l #a$ a%a '!!b*'

5a0,s +ik0ksi.

*,m,s K0ksi a+ala5 :

(RL4 5.5.17, T 4 6R6L K6L, al 119)

B/T = 2.8!494

!$ B/T = 0,1: x ((B/T) - 2,5)

= .84879

*,m,s K0ksi/a

.9873879

#0 = .9874

#a"a p!"$&pa"%a" LCB

; ! = .!F

Lpp = 127.99 mt0

;! x Lpp = .83193mt0

"%%'a Ba#a" Kapal

#ala& al $"$ a"% p!l* #$!$ a#ala b bal$"%-bal$"% '. ;; Ha0al+ 5al. 132 k

as = .4

-. )ahanan )otal

Ksi Ta5aa Ttal Kapal ata, #t& Dapat +itt,ka +ga mE,mla5ka k

C@ + C + Ca + Ca

= .2!97

Caa

= .7

C'=

= .27!7

R' =

= 21.711 K

*t Dias = (1%1F)G*T

= 99.9!2!

C'a$

=

C'*#aa

=

C'a$

+ C'*#aa

C' x 0.5 x A a$la*' x 2 x

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1.2 #$n!m%

9.8mAs2

13.2889

1.18831!

1.4!28.7449

mAs

x A194.94 " 1.2

1!327.7979

('s " Lwl)Ak

1977!8

9.39719!311

7.39719!311

49.7!248

ss $alig$alig& +a p0s $alig$alig

ika.

2.1!97

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2$ = 1$ % (3$1$)C(2a1a)A(3a1a)

= .9289

.9289

.237 (3$1$)= .1

.

.474

i ti+ak +i5it,g

3.1 .31

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)

0ksi ,t,k ta5aa km,+i m,gki skita0 :

siksi ta5a kapal /ag a+a.

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Da/a t0 -gg0ak tama

1. D/ 0F0K)F KP $0P&

Da/a kti ata, H- a+ala5 +a/a /ag +ip0l,ka ,t,k mgg0akka kap

,t,k ma0ik kapal +ga kpata . -05it,ga +a/a kti kapal (H

m,0,t $,k, H;*';*D&T;H;; D; -*? K;-;L& !.2.1 5al. 13 s$a

1 kI = 1.341218!

H- = *t+ias " 's 1 H- = .747

= 92.4!3 KI *t Dias = (1%1F)G*t= 794!.1!!! H- = 99.9!2!3

s = 19.2

9.87!48

2. D/ )B+N4 P5R56 B+R)N BN47BN4 $DP&

;+ala5 +a/a /ag +is0ap l5 p0pll0 +a0i sistm p0p0sa ata, +a/a /a

sistm p0p0sa k p0pll0 ,t,k +i,$a5 mEa+i +a/a +0g (t50,st )

DH- = H-A- Dimaa - = JH " J

a. isisi Lam$,g (JH)

JH =(1t)A(1w)

g5it,g Iak 0iti (w)

Iak 0iti ata, a0,s ik,t m0,paka p0$a+iga ata0a kpata kapal

+ga kpata ai0 /ag m,E, k p0pll0.

Dga mgg,aka 0,m,s /ag +i$0ika l5 Ta/l0 &maka +i+apat :

w = . " #$Il .

= . " .!8 .

= .29

g5it,g T50,st D+,ti at0 (t)

ilai t +apat +ia0i +a0i ilai w /ag tla5 +ikta5,i /ait, :

t = k w ilai K ata0a .7

t = .7 " .29

= .23

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maka sisi lam$,g +apat +ia0i +ga :

JH = (1t)A(1w) (1t) =

= (1.23)A(1.29) (1w) =

= 1.1223211

$. isisi *lati *tati (J00)

Ha0ga J00 ,t,k kapal +ga p0pll0 tip sigl s0w $0kisa0 1.1.1.

(+wa0 '. Lwis-0iipal aal ;05itt,0 5al 12 )

pa+a p0aaa p0pll0 +a ta$,g p0s p0pll0 ii +iam$il 5a0ga :

J00 =1.3

. isisi -0p,lsi (J)

a+ala5 p wat0 i/ /ait, i/ +a0i p0pll0 pa+a saat +ilak,ka

p wat0 tst. ilai/a ata0a 4F7F. Diam$ilJ=!2F

+. #si -0p,lsi (-)

- = JH " J00 " J

= .7191!348

maka& +a/a pa+a ta$,g p0s $alig$alig +i5it,g +a0i p0$a+iga ata

+a/a kti +ga ksi p0p,lsi. Mait, :

DH- = H-A-

= 8239.373!38 KI

= 1149.181 Hp

3 80N4)+N4 D/ PD P5R56 BN47BN4 $6P&

t,k kapal /ag kama0 msi/a t0ltak +i $agia $lakag aka mgala

lsss s$sa0 2F& s+agka pa+a kapal /ag kama0 msi/a pa+a +a0a

kapal mgalami lsss s$sa0 3F.(N-0iipal aal ;05itt,0 5al 131O

-a+a p0aaa ii& kama0 msi t0ltak +i$agia $lakag& s5igga ls

/ag t0Ea+i 5a/a 2F

>H- = DH-AJs Js = .98

= 847.2412 KI

= 11274.!73!2 H-

! 80N4)+N4 D/ P0N440RK +)8 /N4 DP0R+KN

a. BH-s0 : Da/a $0si5 /ag tla5 +ip05it,gka

BH-s0 = >H-AJ6 J6 =

= 1149.181 H-

8239.373!38 KI

$. BH-m0

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Da/a /ag kl,a0 pa+a k+isi maksim,m +a0i mt0 i+,k& +imaa $sa0/

ata, mgg,aka gi ma0gi s$sa0 1F

Da/a BH-s0 +iam$il 8F

BH-m0 = BH-s0A&8

= 12999.347 Hp9!93.387 Kw

Da0i +ata+ata ,tama mt0 i+,k +i atas& maka +ipili5 mt0 i+,k /ag pali

Pis : a BQI

T/p : >42#9 -05it,ga ,lag>t0k : 2 >t0ks

Da/a a" : 972 Kw a)

P,mla5 >ili+0 : 9 #/li+0s =

B0 : 42 mm

>t0k : 17!4 mm $)

*- : 13! *pm =

- : 18 Ba0 =

>H- =

=

Dimsi = =

lgt5 = mm

wi+t5 = mm +) DH- =

5ig5t = mm =

=

!) -# =

=

) -# =

J =

=

BH-#*

=

BH->#*

=

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al +i ai0 ata,

)

ai $0ik,t :

H-

kI

Kt

mAs

g +i5ata0ka l5

0 " J

.9& am$il K = .7

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.797

.71

0a

i

mi+s5ip

).

s

.98

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1F

g ss,ai& /ait, :

+a/a gi :

8!4 Kw

11586.43 H-

&&&6 kI

1042&.&9 H-

&620.48 kI

10219.23 H-

') '

&468.0&04 kI

10014.85 H-

H- A DH-

.793438!94

$

)C!(

0.69

)C/

0,9

)'C/

G

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6yarat Diameter

D ma" p0pll0 = &7 " T = .4719

BP 7 9 Diagram

>$l,m mt,ka ilai Bp1& +ip0l,ka +ata tam$a5a& ata0a lai s$agai $0ik

= 13! 0pm

'a = (1w).'s R +imaa w = &322 13.8

Bp1 =

Ea+i &1739.SBp1 =

-0tama tama /ag +ilak,ka a+ala5 mmp0+iksi s0i $0apa saEa /ag +ig,aka

+a +ipili5 s0i B3& B4& +a B t,k m+apatka ilai +a0i Bp1& maka +i$,t,5ka

('a) s$sa0 13.8 kt

>tla5 mt,ka/a& maka lagka5 slaE,t/a a+ala5 m+apatka ilai Bp1

$0ik,t :

Bp1 : N ; 6P

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1=>o 9o9o :

B44 . 1.79 181.27

B4 . 1.81 183.29

B47 . 1.8 182.28

B48 . 1.77 179.24

B41 . 1.72 174.18

B0ik,t ii a+ala5 t5 pm$aaa +iag0am Igig B >

>tla5 +i+apatka ilai -AD +a 1AP& maka +ilak,ka p05it,ga D& D$& V$

D (t) = 'a"V

D$ (t) = .9! D (sigl s0w)+iamt0

D$ (t) = .98 " D (twi s0w)

V$ = D$"ilai +iplt

'a

=

aka ilai -AD$ +a J aka +ip0l5 +ga mm$aa km$ali k +iag0am-AD$ = +ip0l5 +a0i pm$aa

)ypepropeller

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J = +ip0l5 +a0i pm$aa

1/Jb= 0.009875 " V$

Do (ft)Db (ft)

b 1/Jb P/Dbsingle screw

B44 17.34 1!.!4 174.118987 1.7184 0.87

B4 17.3 1!.83 17.99493!7 1.737! 0.8:0

B47 17.43 1!.74 174.98734177 1.728 0.8:0

B48 17.14 1!.4! 172.788!8 1.!992 0.900

B41 1!.!! 1.99 1!7.2112!8 1.!12 0.930

!. 8enentukan Diameter Propeler

Do $%t&

D $%t& D $m&

D ma; $m& Dmin $m&

single scre@ single scre@

B44 17.34 1!.!4 .7 .

B4 17.3 1!.83 .13 .

B47 17.43 1!.74 .1 .

B48 17.14 1!.4! .2 .

B41 1!.!! 1.99 4.87 .

'. 8enghitung KaAitasi

B0ik,t ii a+ala5 lagka5 lagka5 ,t,k mt,ka kaitasi ti+ak/a

1. t,ka ilai W&7* t0l$i5 +a5,l,

W&7* =

(Principles naval architecture, hal

Dimaa :

5 Pa0ak ata0a #t0 p0s +ga sa0at

= .83 m +ip0l5 +a0i gam$a0 lis pla

Typepropeller

)ypepropeller

-05it,ga kaitasi p0l, +ilak,ka +ga t,E,a ,t,k mmastika s,at,

m/$a$ka k0,saka atal t05a+ap p0pll0. -05it,ga kaitasi ii +ga m

(1&882%19&!2(5))A'a2%4&83!2D2

ilai W&7* ii +ig,aka ,t,k mgta5,i ilai agka kaitasi pa+a +iag0am $,00il

+ga k,0a m05at s5ip p0pll0.

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enis Prop e=o o e d p $%t2&

B44 .4 217.!!179!1!14 97.94788273 97.94788273 84.99!17

B4 .! 222.29198228 133.317189 133.317189 11!.18!

B47 .7 22.1!47!48 1!.74237 1!.74237 143.!2

B48 .9 212.82183184 191.421!49 191.421!49 1!4.899

B41 1. 2.9783!!!!7 211.19378 211.19378 18.21!9

= 2.2!!!!!!7 *ps

Vr2 ) Cc itungan

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t :

,t,k +sig p0pll0&

ilai +a0i a+a sp+

+ga 0,m,s s$agai

+a5 +a0i 's (kpata

w +isplamt Uts

0pll0.

s5igga +ip0l5 5a0ga

a +ilak,ka p05it,ga

a +ilak,ka p05it,ga

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.987

0is

0pll0 maksimal

ka k +iag0am Bp

$alik k +iag0am Bp

0 p0pll0 pa+a k+isi

p wat0

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$alik k +iag0am Bp

b

0.:3

0.:2

.!1

.!

.9

D J Dma;

tak ss,ai

tak ss,ai

tak ss,ai

tak ss,ai

tak ss,ai

p0pll0 /ag kita pili5

182, pers 61)

0pll0 $$as +a0i kaitasi /ag

gg,aka Diag0am B,00ilXs.

l +iptgka

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p $m2& Va $m=s&

7.897 !.!91

1.794 !.!91

13.344 !.!91

1.32 !.!91

1!.743 !.!91

itasi

?'AZ

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0N4N0 PR5P00R 8)"N4

Data kapal /ag +ip0g,aka a+ala5 : Da/a = !93 KI

t = .23

w = .29

= 19.2 kt = 9.87!48 mAs

= 12

Data p0pll0 /ag +i+apatka:

Tip -0pll0 = B48

= 1!.4! t = .2

= 0.900

J p0pll0 = .!

*pm -0pll0 = 13!. 0pm

)ahanan total pada saat clean hull $ersih tanpa kerak&

= 21.71 k

)ahanan total pada saat serAice lamung telah ditempeli oleh %ouling

= 99.9! k

+N) DN 68B5

a = Kstata

[ = kstata

KT = Ksi 6a/a D0g (t50,st) Balig$aligP = Ksi 6a/a ;+a+ Balig$alig

K\ = Ksi T0si BaligBalig

\ = T0si

P0R)+N4N

1. 8enghitung Koe%isien

*t=

*t=

348.32 !1.7

.1!1 .9

$iasa/a P it, ilai/a

's

ai0 la,t kgAm3

D$(m)

(-AD$)

*tt0ial

*ts0i

. " " #t " > " s2

a " s2

]t0ial

= *t A 's2

]t0ial =

]s0i

=

2. 8enghitung KoeLsien [

[ =] A ^(1t) (1w)2 D2_

[t0ial

= [s0i

=

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3. 8emuat KurAa huungan K)7>

P

. . KT =.1 .1 . .1

.2 .4 .21 .2

.3 .9 .4! .

.4 .1! .83 .9

. .2 .129 .1

.! .3! .18! .21

.7 .49 .23 .29

.8 .!4 .33 .38

.9 .81 .418 .48

1 1 .1! .9

!. Perhitungan Nilai Propeller

-AD$ .9

P KT 1K\ J

.1 .3994! .4773 .1199!3

.2 .3247! .437!1 .23!138

.3 .28939 .392989 .3472!3

.4 .24398! .3441!! .41131

. .199428 .291784 .43!7

.! .12784 .23!49 .!1!!!8

.7 .147 .17892 .!779

.8 .321 .11987 .87!79

.9 .41 .9711 .13287!

KT = [ " P2

P2 KTt0ial KTs0i

-mili5a tip p0pll0 +ilak,ka +ga a0 mma0iasika -AD km,+ia +i pl

k,0a p wat0 tst s5igga +i+apat +ata KT& K\ & P +a J

.2 .4 .! .8 1 1.2

.2

.4

.!

.8

1

1.2

KT t0ial KT s0i

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1

titik ptg P titik ptg Kt titik ptg 1K` titik pt

.! .2 .3 .!

.! .1 .2 .3 .!

.! .2 .2 .3 .!

.! .3 .2 .3 .!

.! .4 .2 .3 .!

.! . .2 .3 .!

.! .! .2 .3 .!

.! .7 .2 .3 .!

titik ptg P titik ptg Kt titik ptg 1K` titik pt

.9 .21 .32 .!

.9 .1 .21 .32 .!

.9 .2 .21 .32 .!

.9 .3 .21 .32 .!

.9 .4 .21 .32 .!

.9 . .21 .32 .!

.9 .! .21 .32 .!

.9 .7 .21 .32 .!

P : .!

KT : .2

J : .!

K\ : .3

Ea+i pa+a k+isi "lean ull +ip0l5 ilai s$agai $0ik,t :

Ea+i pa+a k+isi Rough ull +ip0l5 ilai s$agai $0ik,t :

.1 .2 .3 .4 . .! .7 .8 .9 1.1

.1

.2

.3

.4

.

.!

.7

.8

.9

1K) M K

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P : .9

KT : .21

J : .!

K\ : .32

=

'a 'a =

P D= 2.223137

= 133.3882 0pm

='a *pm ma"

P D

= 2.2!817

= 13.!49 0pm

gi p0pll0 p0pll0\

DH- >H-

(0pm) (0pm) (0ps) (H-) (H-) (KI)

.

1 1 .1!7 2713.392 284.2 2897.98 3

2 2 .333 183.!7 2272.13 23183.81 27

3 3 . 2442.2! 7!!8.4 7824.3! 92

4 4 .!!7 43414.2!9 1817!1.7 1847.48 218

.833 !7834.79 32.9 3!2247.3 42!

! ! 1. 97!82.1 !13443.!2 !29!2.87 73!

7 7 1.1!7 1329!.198 97412.74 994.8! 11!9

8 8 1.333 173!7.7 14488.7 14837!3.8 174!

9 9 1. 219784.73 27372.21 2112!24.7 248

1 1 1.!!7 271339.18 2841!.7 289797!.27 349

11 11 1.833 32832.47 378!2.29 3872!.42 438

12 12 2. 39728.419 49748.94 773. 891

13 13 2.1!7 48!3.214 !2391!.79 !3!!83.87 749

133.38 133 2.223 482718.489 !7389!2.1 !87!492.3! 89

13! 13! 2.2!7 18!8.947 7143937.17 7289731.8 87!

gi p0pll0 p0pll0\

DH- >H-

(0pm) (0pm) (0ps) (H-) (H-) (KI)

.

1 1 .1!7 2894.28 329.3 391.17 4

2 2 .333 1177.138 24234.81 24729.4 29

3 3 . 2!48.!1 81792.48 834!1.72 98

4 4 .!!7 4!38.3 193878.48 19783.18 233

.833 7237.11 378!!8.9 38!39!.84 4

! ! 1. 14194.24 !4339.8! !!7!93.73 78!7 7 1.1!7 141819.94 139!7.4! 1!272.92 1247

8 8 1.333 18234.213 1127.81 182!81.44 18!2

+sig +iti

s0i

BH-#*

Ta$l +iatas m0,paka p05it,ga +a/a msi pa+a p,ta0aa t0tt, +ga k+isi lamasi5 $0si5 (la 5,llA+sai) ti+ak a+a ka0at ma,p, $iatag la,t /ag mmpl pa+a(,lig)& pa+a k+isi s$alik/a (0,g5 5,llAs0is) t0+apat

BH-#*

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9 9 1. 234437.1 228397.2 2234!!.3 2!1

1 1 1.!!7 289428.48 32931.2 391174.!9 3!37

11 11 1.833 328.434 432!!.44 411433.1 484

12 12 2. 41!77!.98 234718.87 34149.8! !284

13 13 2.1!7 489134.94 !!484.8 !79131.79 799

13.! 13! 2.2! 32182.2! 731!.1 7773!.28 9!7

13! 13! 2.2!7 332!.87! 7!2199.!4 777713.92 9148

0ngine 0nAelope

gi T/pgi >p+

-w0

B0 42 mmL1 13! 972

L3 11 823

>t0k 17!4 mmL2 13! 778

L4 11 !7

BH- >a a0gi = 9!7.42 kI b = 13!. 0pm

Da0i BH- >a a0gi +iam$il gi ma0gi s$sa0 1F

BH- gi ma0gi = 9!7.4191 kI = 131F BH-m0 gi

La/

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m

1&!

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[ " P

2

tka +ga

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g U

g U

untuknilai K)

trial

untuknilai K)serAice

KT

K\J

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!.!91 mAs

13!

*-

(F) (F)

7 .

1 .39

22 1.33

29 3.1

37 !.1

44 1.!3

1 1!.87

9 2.19

!! 3.8!

74 49.2

81 !.48

88 8.1

9 18.9

98 11!.74

1 123.7

*-

(F) (F)

7 .

1 .42

22 1.42

29 3.3!

37 !.!

44 11.341 18.

9 2!.87

BH-#*

$,g kapal /aglam$,g kapal

BH-#*

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!! 38.2!

74 2.48

81 !9.8

88 9.!8

9 11.29

1 13.84

1 132.

250

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Propeller Dra@ing $eG dG p&

Data teknis propeller yang diutuhkan untuk perhitungan H

G k,0a ,tama p0pll0 :

T/p = B48 Pa0i Ea0i ( * ) =

P,mla5 +a, (c) = 4 Da, ; A ; =

-,ta0a () = 13! 0pm -it5 0asi (-AD) =

Diamt0 (D) = .2 m isisi (J) =

G Kt0aga :

c = P,mla5 Da, -0pl0

D = Diamt0 -0pl0

;A; = "pa++ 0ati

;A; .8 2.1

c 4

D .2 mt0

0A* (#AD)(cA(; aA $A ;0 B0 #0 ;0

.2 1.!!2 .!17 .3 .2! .4 1.772939 1.9393

.3 1.882 .!13 .3 .4!4 .3 2.7!24 1.23!73

.4 2. .!1 .31 .42 .3 2.18!838 1.314289

. 2.12 .8! .3 .34 .2 2.29!4! 1.34249

.! 2.187 .!1 .389 .278 .2 2.332982 1.3883

.7 2.144 .24 .443 .21! .1 2.287112 1.198447

.8 1.97 .4!3 .479 .14 .1 2.11498 .972993

.9 1.82 .31 . .92 . 1.!8799 .92347

1 . . . .3 .

t,k -d (T5 Dsig a0i >0w -0pll0 5lm.72)

t,k -e

. g ,g a a ms a, p0p 0Dimsi p0pll0 mlip,ti a0& $0& 0& +a >0. ilaiilai +i atas +ip0l5 +a0i ta$l

. g ,g 0 a aTitiktitik k0+iat /ag +i$,t,5ka l5 p0l +apat +i5it,g +ga 0m,lasi /agl5 'a 6t t al (1973) +a 'a 0w -0pll0 5lm.72

>tla5 mgta5,i ilai masig masig (0&a0&$0 +a >0) +iatas& maka lagka5 pg+ilaE,tka pa+a pt,a pampag kt$ala tiap $agia +a, mgg,aka 0,ta$l +i$awa5 ii :

M;#

= '1(t

ma"f t

l.)

MB;#K

= ('1% '

2) (t

ma"f t

l.)

M;#= '1(tma"f tl.)

MB;#K

= ('1% '

2) ( t

ma"f t

l.)

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1

6

/R -1 -0.95 -0.9 -0.8 -0.7 -0.: -0.5

0.15 0.3 0.282 0.2:5 0.23 0.195 0.1:1 0.128

0.2 0.282: 0.2:3 0.2 0.19:7 0.157 0.1207 0.088

0.25 0.2598 0.2372 0.2115 0.1:51 0.12: 0.0899 0.0579

0.3 0.230: 0.20 0.179 0.1333 0.093 0.0:23 0.037:

0. 0.1:7 0.12 0.0972 0.0:3 0.0395 0.021 0.011:

0.5 0.0522 0.02 0.033 0.019 0.01 0.00 0.0012

0.: 0 0 0 0 0 0 0

0.7 0 0 0 0 0 0 0

0.8 0 0 0 0 0 0 0

0.9 0 0 0 0 0 0 0

1 0 0 0 0 0 0 0

6

/R 0 0.2 0. 0.5 0.: 0.7 0.8

0.15 0 0.009: 0.038 0.0:15 0.092 0.132 0.187

0.2 0 0.009 0.030 0.052 0.080 0.118 0.1:85

0.25 0 0.0031 0.022 0.017 0.0::9 0.1008 0.1:5

0.3 0 0.0027 0.018 0.03 0.0503 0.079 0.1191

0. 0 0 0.0033 0.009 0.0189 0.0357 0.0:37

0.5 0 0 0 0.0008 0.003 0.0085 0.0211

0.: 0 0 0 0 0 0 0.000:

0.7 0 0 0 0 0 0 0

0.8 0 0 0 0 0 0 0

0.9 0 0 0 0 0 0 0

1 0 0 0 0 0 0 0

6

/R -1 -0.95 -0.9 -0.8 -0.7 -0.: -0.5

0.15 0 0.05 0.1325 0.287 0.28 0.5585 0.:77

0.2 0 0.0: 0.155 0.30: 0.535 0.582 0.:995

0.25 0 0.0725 0.15:7 0.3228 0.7 0.:05 0.718

0.3 0 0.08 0.1:7 0.33: 0.885 0.:195 0.7335

0. 0 0.0905 0.181 0.35 0.50 0.:353 0.7525

0.5 0 0.095 0.18:5 0.35:9 0.51 0.:39 0.758

0.: 0 0.09:5 0.1885 0.3585 0.511 0.:15 0.753

0.7 0 0.0975 0.19 0.3: 0.51 0.: 0.75

0.8 0 0.0975 0.19 0.3: 0.51 0.: 0.75

0.9 0 0.0975 0.19 0.3: 0.51 0.: 0.75

1 0 0.0975 0.19 0.3: 0.51 0.: 0.75

6

Dimaa ilai '1+a '

2(ta$,lat+ ,tis +p+t 0A* a+ -) m0,paka kst

$isa +ili5at pa+a ta$l $0ik,t :

*

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/R 0 0.2 0. 0.5 0.: 0.7 0.8

0.15 1 0.97: 0.8825 0.8055 0.7105 0.5995 0.52

0.2 1 0.975 0.8875 0.817 0.7277 0.:19 0.777

0.25 1 0.9751 0.8899 0.8259 0.715 0.:359 0.982

0.3 1 0.975 0.892 0.8315 0.752 0.:505 0.513

0. 1 0.9725 0.8933 0.835 0.7593 0.:59 0.522

0.5 1 0.971 0.888 0.8275 0.778 0.:3 0.5039

0.: 1 0.9:9 0.879 0.809 0.72 0.:0: 0.:2

0.7 1 0.9:75 0.8:: 0.785 0.:8 0.5:15 0.1

0.8 1 0.9:35 0.852 0.7:35 0.:55 0.52:5 0.37:5

0.85 1 0.9:15 0.85 0.755 0.:55 0.51: 0.3::

0.9 1 0.9: 0.8 0.75 0.: 0.51 0.3:

1 1 0.9: 0.8 0.75 0.: 0.51 0.3:

K

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0.9 . .32 .!87 .131 .1843 .2313 .2711

1 . . . . . . .

0A* .2 .4 . .! .7 .8

0.2 .18373 .184 .1!8! .19!! .14847 .1341 .11873

0.3 .1!2! .192 .14749 .1412 .1349 .118! .1281

0. .141! .137!7 .12!93 .11941 .1117 .9834 .82910.5 .1248 .11!99 .1!99 .9979 .9 .7849 .!32

0.: .994 .9!31 .8737 .841 .717 .!23 .498

0.7 .7831 .777 .!782 .!147 .37 .4397 .3242

0.8 .723 .14 .487! .43!9 .374! .313 .21

0.9 .3!14 .347 .33! .2711 .2313 .1843 .131

1 . . . . . . .

D6)RB+6 P)"

D : .2 m

-AD : .9

- : 4.18 m

-A2 : .719427 m

0A* FHA2

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2.1

.8

.9

.!

B0 t=s0 #0;0 0A* #0;0

.!228 .183732 .!793 .2 .4933

.72!!8 .1!2!48 .77!9 .3 .!1432

.7!78 .141!4 .87248 .4 .73984

.81494 .1248 .9397 . .829917

.973 .9939! 1.24179 .! .924783

1.13191 .78312 1.88!! .7 1.133

1.!!17 .7228 1.1284 .8 1.7127!

.843799 .3!144 1.921 .9 1.917

1

$0ik,t:

i$0ika

a0i

0Eaa,sa +a

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-0. -0.2 0

0.0955 0.03:5 0

0.0592 0.0172 0

0.035 0.008 0

0.0202 0.0033 0

0.00 0 0

0 0 0

0 0 0

0 0 0

0 0 0

0 0 0

0 0 0

0.85 0.9 0.95 1

0.223 0.2:2 0.315 0.38:

0.2 0.2353 0.2821 0.35:

0.177 0.20:8 0.2513 0.325:

0.15 0.17: 0.218: 0.2923

0.0833 0.1088 0.1:7 0.2181

0.0328 0.05 0.0778 0.1278

0.0022 0.00:7 0.01:9 0.0382

0 0 0 0

0 0 0 0

0 0 0 0

0 0 0 0

-0. -0.2 0

0.7805 0.93: 1

0.798 0.9: 1

0.8139 0.9519 1

0.82:5 0.9583 1

0.815 0.9:5 1

0.85: 0.9:39 1

0.82: 0.9:13 1

0.8 0.9: 1

0.8 0.9: 1

0.8 0.9: 1

0.8 0.9: 1

ta /ag

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0.85 0.9 0.95 1

0.3::5 0.2: 0.13 0

0.3905 0.28 0.15: 0

0.108 0.302 0.1758 0

0.2:5 0.3197 0.189 0

0.335 0.3235 0.1935 0

0.135 0.305: 0.175 0

0.3775 0.272 0.185 0

0.33 0.2337 0.12 0

0.2925 0.2028 0.105 0

0.283 0.195 0.1 0

0.2775 0.19 0.0975 0

0.2775 0.19 0.0975 0

.4 .2

.1877 .31!

.328 .37

.!23

.8 .9 .9 1

.3!74! .43232 .1831 .!49

.233 .28!2! .3 .4742

.11792 .142 .27!7 .387

.392 .!24 .9373 .1397

.219 .!!! .1!8 .3797

.4 .2

.177 .17!71 .18373

.13771 .1!4 .1!2!

.1197 .13!4 .141!

.1188 .11!13 .1248

.837 .9 .994

.!78 .718 .7831

.487 .494 .723

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.33! .347 .3!14

. . .

.8 .9 .9 1

.1849 .941 .849 .!41

.9287 .8!2 .!!3 .474

.731! .!12 .481! .388.377 .4284 .34! .14

.3774 .277 .1!44 .38

.284 .183 .971 .

.1!74 .11!1 .!1 .

.13 .!87 .32 .

. . . .

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< T$

< a' !$ #aa

< 4aa p!!"a"aa"

,la0s&

4$a&b$l @2 = 2.3

!$"%%a, T!%a"%a" %!! a"% #$$D$"a" (')