16
) ( 5 2 !"#$ 88 &’( 23 * 37 23 1 2 3 ,- ./ -0 . 10 ,- , 0 2 3 10 4 -0 ,- ./ -0 . 10 ) ! " # : 14 / 02 / 1388 )*+ #! , : 23 / 09 / 1388 ( /0 *5 67 8.$ 9:; <=0$ >?. 6:$ 9- @.= .A B& >7.$B C ’B B# DB E5 4 G$ H .# D $ $. , 9 I . 7 6 & 8.$ D7 9&$ ,$ .17B7 B# 9K" ’= ./ .; . 8.$ & & D.7LM NO: .P$ Q? 9B BR EK # :KS >?. . T7B D.# C 67 U(4 EV D W, ./ .; .# ? # 7 &$ 6 :; U 9B B3 9 # 8.$ 9 . - 7 9 7 U(4 T &$ "?. U .$ C ? # 7 E5 > # 7 QXM U(4 T D #.$ 5 7 Y$ ? " # .# ? # C 9&( , !0 ZM 6 # . ! : & 8.$ E5 >7.$ C [ "?. U&$ & \, 5 A Novel Way for Crack Detection in Rotors, Using Mode Shape Changes M. Raghebi M. Hoseinzadeh A. Farshidianfar Mech. Eng. Group Ferdowsi Univ. of Mashhad School of Eng. Islamic Azad Univ., Mashhad Branch Mech. Eng. Group Ferdowsi Univ. of Mashhad ABSTRACT In this article, a non-destructive method for the frequency analysis and multi-crack detection in rotating shafts is presented, using transfer matrix method (TMM) and based on the Timoshenko beam theory. The cracks can be placed in different angles with respect to each other. The presence of cracks in structures change the local flexibility and results in reduction of natural frequency. The TMM is exerted for the frequency analysis of the shafts with discrepant boundary conditions. The resultant frequencies are used for requiring the mode shapes of the shaft corresponding to the two perpendicular planes (x-z and y-z). Subtracting these two mode shapes gives the position of the crack or cracks. Finally, the required frequencies by TMM are compared with some available experimental results. Close adaptation between these results is representing the high accuracy of the transfer matrix method. Key Words: Cracked Shaft, Frequency Analysis, Mode Shape, Transfer Matrix Method (TMM), Overhang Shaft 1 - 0 ) 1=M ,"7 :( [email protected] 2 - H,? ) ! !.10XM 1# W ( : [email protected] 3 - D.? D0 4-Transfer Matrix Method (TMM) 5-Overhang Shaft

23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

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Page 1: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

و هوا فضا و رفتار مكانيكي مواد(مجله مكانيك 3723 الي23، از صفحه88، تابستان2، شماره5، جلد)سازه

، دواريهامحوردر براي رديابي تركديجديروش

به كمك تغييرات شكل مد3مهدي راغبي2محمد حسين زاده1انوشيروان فرشيديان فر

گروه مهندسي مكانيك دانشگاه فردوسي مشهد

و مهندسي دانشكده فني مشهد، واحددانشگاه آزاد اسالمي

گروه مهندسي مكانيك دانشگاه فردوسي مشهد

)23/09/1388:؛ تاريخ پذيرش14/02/1388:خ دريافتتاري(

چكيده

در،در اين مقاله و تشخيص موقعيت ترك هـاي دوار، بـا اسـتفاده از روش مـاتريس محـور روشي غير مخرب جهت تعيين فركانستيتيو بر اساس تئور4انتقال ا. ارائه شده است،موشنكوير م،محورنيدر مي ترك ها ختلفي نسبت بـه يكـديگر توانند تحت زواياي

نتـايج. فركانس طبيعي را به دنبال خواهـد داشـت كاهشو داده تغيير را انعطاف پذيري محلي ها محوردر وجود ترك. قرار گيرندها حاصل از اين روش براي وي متنوعي مثال ا مورد بررسي قرار گرفته در.ت ترك به دست آمـده اسـتيل موقعين تحلي به كمك

ازيت، نتاينها هايبا نتاس انتقالي به كمك روش ماتريل فركانسي تحلج حاصل سه شده كه توافقي مقاي تجربيج حاصل از پژوهشميب . باشدين پاسخ ها نشان دهنده صحت روش به كار برده شده

5 اورهنگمحور، دار، تحليل فركانسي، مد شيپ، روش ماتريس انتقال تركمحور: كليديواژه هاي

A Novel Way for Crack Detection in Rotors, Using Mode Shape Changes M. Raghebi M. Hoseinzadeh A. Farshidianfar

Mech. Eng. Group Ferdowsi Univ. of Mashhad

School of Eng. Islamic Azad Univ., Mashhad Branch

Mech. Eng. Group Ferdowsi Univ. of Mashhad

ABSTRACT In this article, a non-destructive method for the frequency analysis and multi-crack detection in rotating shafts is presented, using transfer matrix method (TMM) and based on the Timoshenko beam theory. The cracks can be placed in different angles with respect to each other. The presence of cracks in structures change the local flexibility and results in reduction of natural frequency. The TMM is exerted for the frequency analysis of the shafts with discrepant boundary conditions. The resultant frequencies are used for requiring the mode shapes of the shaft corresponding to the two perpendicular planes (x-z and y-z). Subtracting these two mode shapes gives the position of the crack or cracks. Finally, the required frequencies by TMM are compared with some available experimental results. Close adaptation between these results is representing the high accuracy of the transfer matrix method.

Key Words: Cracked Shaft, Frequency Analysis, Mode Shape, Transfer Matrix Method (TMM), Overhang Shaft

[email protected]): نويسنده پاسخگو(دانشيار-1 [email protected]:)عضو باشگاه پژوهشگران جوان(كارشناس ارشد-2 دانشجوي دكتري-3

4-Transfer Matrix Method (TMM) 5-Overhang Shaft

Page 2: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

XY

XY

iPi

ij

N

ir

xy

l

r

[1]

[2]

[3]

1-Dimarogonas and Pipetis 2-Papadopoulos

a

A

cij

E

G

I

)(J

iNK

k

M

iP

Q

iu

ZYX

ZYX

Page 3: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

[4]

]

[

]

[

]

[

]

[

1-Sekhar 2-Gasch 3-Laval Rotor 4-Chondros 5-Rayleigh Quotient 6-Hu-Washizu-Barr

]

[

]

[

]

[

]

[

]

[

7-Bachschmid 8-Tsai and Wang

Page 4: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

A-A

iP6,,...2,1i

]

[iu

ai

1-Paris

,0

a

ii

u J ( ) dP

)(J

.1

1)(

26

1

26

1

26

1

2

dXK

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J

ii

ii

ii

b

b

E

),(h

FK NiiN

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iP)/( hFNA

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2

dXdJPP

cb

b

a

jiji

[13]

44c45c55c33c

B

ZYX

ZYX

Z

ZZ

Page 5: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

XY

XY

A

I

,

2

1

2

0

222

ZdX

YAGkIEU

Y

L

XYX

,2

1

0

2222ZdIYXAT

L

YX

Gk

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XY

XY

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:

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XT

Y

X

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XT

Y

XT

T

.cossin

sincos

tt

ttT

ZYX

,02 2YX

GkYXYX

,02 2XY

GkXYXY

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I

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I

AGkE

XY

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0

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YhYgYfXeXdXcXbXaX iv

,0....

XhXgXfYeYdYcYbYaY iv

EGka

22

, EGk

b ,

IE

A

EGkc

242

, IE

A

EGkd

226

EGke

2,

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22 ,

IE

A

EGkg

24 32

, EGk

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Page 6: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

,0

....

XX

XYYYYYvi

Y

hg

fedcba

.0

....

YYY

XXXXXvi

X

hgf

edcba

,, tieZxtZX

,, tieZYtZY

1i

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,0xsixriyqypyiv

,2222

GkGkEEp

,6 422224222

EGkEGkEGkIE

A

IE

Aq

,22

GkEr

.442 3232

EGkEGkIE

As

,Zir eAiAZx

.Zir eBiBZy

ArAiBrBi

.0

00

00

00

00

242

242

224

224

qpsr

qpsr

srqp

srqp

.,,, 4321 ii

Bi=-ArBr=Ai12Br=-Ai

Bi=Ar34

,88776655

44332211

qAqAqAqA

qAqAqAqAZxr

,88776655

44332211

qBqBqBqB

qBqBqBqBZxi

,88776655

44332211

qBqBqBqB

qBqBqBqBZyr

,88776655

44332211

qAqAqAqA

qAqAqAqAZyi

,sin,cos,sinh,cosh 24231211 zqzqzqzq

.sin,cos,sinh,cosh 48473635 zqzqzqzq

,847748635536

423324211112

qpAqpAqpAqpA

qpAqpAqpAqpAZry

,847748635536

423324211112

qpBqpBqpBqpB

qpBqpBqpBqpBZiy

,847748635536

423324211112

qpBqpBqpBqpB

qpBqpBqpBqpBZrx

847748635536

423324211112

qpAqpAqpAqpA

qpAqpAqpAqpAZix

Page 7: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

2 2

1 1 2 21 2

2 2

3 3 4 43 4

p , p ,k G k G

p , p .k G k G

,, yyxx IEMIEM

., xyyx yGAkQxGAkQ

.,,,,,,,

,,,,,,,,T

ixiyixirxryrxr

iyixiyiryrxryr

MQyMQy

MQxMQxU

1ii UEU

E

,22l

xlr Qcxx

,33l

ylr Qcyy

,4555l

yl

xl

xr

x McMc

,4544l

xl

yl

yr

y McMc

,lx

rx QQ

,ly

ry QQ

,lx

rx MM

.ly

ry MM

rl

c22c33

c44c45c55

,lr UHU

H

C

sY

TMM

a,0jsj UTU

b,011 jsj UTU

c.1 sjjsj UHU

.01

01 jjj UTHTU

T

D

Page 8: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

,lr xx

,lr yy

,lr xx

,lr yy

ly

llry

rrlx

rx xAGkxAGkorQQ ,

lx

llrx

rrly

ry yAGkyAGkorQQ ,

,lx

rx MM

.ly

ry MM

,111 l

xrll

yr

y QAAGk

.111 l

yrll

xr

x QAAGk

,lr USU

S

E

,... 0112221

2311 UESETHTEESEU nnnn

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0

2221

1211 U

QQ

QQU n

0

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Q21

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1234123 ,,,,,, ppp4p

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Page 9: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

mL 1mD 03.0

GpaE 2003.03/7860 mkg

Da0.10.3 0.5

lZ0.10.20.9

Y0000

80

90

100

110

120

130

140

150

160

170

180

0 10 20 30 40 50

Rotational speed (Hz)

Nat

ural

fre

quen

cy (

Hz) z2/L=0.2

z2/L=0.4

z2/L=0.5

z2/L=0.7

1.0Da5.0Da

300

310

320

330

340

350

360

370

380

390

400

410

420

0 10 20 30 40 50Rotational speed (Hz)

Nat

ural

fre

quen

cy (

Hz)

z2/L=0.2

z2/L=0.4

z2/L=0.5

z2/L=0.7

1.0Da5.0Da

80

90

100

110

120

130

140

150

160

170

180

0 10 20 30 40 50

Rotational speed (Hz)

Nat

ural

fre

quen

cy (

Hz)

z2/L=0.2

z2/L=0.4

z2/L=0.5

z2/L=0.7

3.0Da5.0Da

Page 10: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

300

310

320

330

340

350

360

370

380

390

400

410

420

0 10 20 30 40 50Rotational speed (Hz)

Nat

ural

freq

uenc

y (H

z) z2/L=0.2

z2/L=0.4

z2/L=0.5

z2/L=0.7

3.0Da5.0Da

Hz10

Hz10

1-Backward Whirling 2-Forward Whirling

Y0321 0

Hz

X-ZY-Z

0.0E+00

5.0E-07

1.0E-06

1.5E-06

2.0E-06

2.5E-06

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

Z(m)

Y-Z plane

X-Z plane

Rel

ativ

e am

plitu

de o

f fu

ndam

enta

l mod

e

X-ZY-Z

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X-ZY-Z

0.E+00

5.E-08

1.E-07

2.E-07

2.E-07

3.E-07

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

Z(m)

Dev

iatio

n of

1st

mod

e in

di

ffer

ent p

late

s (X

-Z &

Y-Z

)

X-Z

Y-Z

123

X-ZY-Z

0.E+00

5.E-07

1.E-06

2.E-06

2.E-06

3.E-06

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

Z(m)

Y-Z plane

X-Z plane

Rel

ativ

e am

plitu

de o

f fu

ndam

enta

l mod

e

X-ZY-

Z

0.E+00

2.E-08

4.E-08

6.E-08

8.E-08

1.E-07

1.E-07

1.E-07

2.E-07

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

Z (m)

Dev

iatio

n of

1st

mod

e in

di

ffer

ent p

late

s (X

-Z &

Y-Z

)

X-Z

Y-Z

]

[

Crack positions

Crack positions

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[15]

L=

Do=

[15]

Crack data Case No.

ta /2 2

ta /1 1

0.38077 0.350 0.19043 0.207 1

0.63460 0.350 0.25385 0.207 2

0.19043 0.350 0.38077 0.207 3

0.25385 0.350 0.63460 0.207 4

(Hz)

Experimental [15] TMM

3

2

3

2

Case No.

835.00 382.50 842.86 378.92 No

crack 834.81 382.16 842.23 378.81 1 834.48 381.48 840.85 378.64 2 834.50 382.01 842.16 378.61 3 833.50 381.10 840.61 377.89 4

[16]

40cr

[16]

mm

L=mm

L1=mm

L2=

L3=N/m2 E

kg/m3mm

d1=mm

d2=e=

L1

1-Doppler Signal Laser Vibrometer

Page 13: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

TMM

a

b

c ]

[

Hz

TMM

3

2

1

ha

2Le

1054.02 584.21 98.37 0.21 (a) 0.789 1049.71 583.41 97.3 0.41 (b) 0.789 1054.16 584.24 98.40 0.18 (c) 0.789

Experimental [16]

3

2

1

ha

2Le

1051.64 583.84 97.34 0.21 (a) 0.789 1032.64 580.87 93.04 0.41 (b) 0.789 1053.58 584.71 97.99 0.18 (c) 0.789

-

X-ZY-Z

[12]

]

[

1

Dimarogonas, A.D. and Paipetis, S.A., Analytical Methods in Rotor Dynamics , Applied Science Pub., London, 1983.

2

Dimarogonas, A.D., Vibration of Cracked Structures: A State of the Art Review , Eng. Fracture Mech., Vol. 55, No. 5, pp. 831- 857, 1996.

3

Papadopoulos, C.A. and Dimarogonas, A.D., Coupled Longitudinal and Bending Vibrations

Page 14: 23 37 * &’( ! #$ ˚˜ ˆprofdoc.um.ac.ir/articles/a/1014757.pdf · 23 37 * 23 &’( ˝88 ! "#$ ˝2 ˚˜ ˝5 ˆ ˙ ˝( ˇˇˆ ˙˝˛ ˚ 3ˇˆ˙ ˝ ˛˚ 2 1 ˘ˆ,- ./ ˆ-0 ˘ . 10

of a Rotating Shaft with an Open Crack , J. Sound and Vibration, Vol. 117, No. 1, pp. 81- 93, 1987.

4

Papadopoulos, L.A. and Dimarogonas, A.D., Coupling of Bending and Torsional Vibration of

a Cracked Timoshenko Shaft , Ingenieur-Archiv, Vol. 57, No. 4, pp. 257- 266, 1987.

5. Papadopoulos, C.A. and Dimarogonas, A.D., Coupled Vibration of Cracked Shafts, J.

Vibration and Acoustics , Vol. 114, No. 1, pp. 461- 467, 1992.

6. Sekhar, A.S., Vibration Characteristics of a Cracked Rotor with Two Open Cracks , J. Sound and Vibration, Vol. 223, No. 4, pp. 497- 512, 1999.

7. Gasch, R., Dynamic Behaviour of the Laval Rotor with a Transverse Crack , Mech. Systems and Signal Processing, Vol. 22, No. 1, pp. 790- 804, 2008

8. Chondros, T.G. and Labeas, G.N. Torsional Vibration of a Cracked rod by Variational Formulation and Numerical Analysis , J. Sound and Vibration, Vol. 301, No. 2, pp. 994- 1006, 2007.

9. Sekhar, A.S., Multiple Cracks Effects and Identification , Mech. Systems and Signal Processing, Vol. 22, No. 1, pp. 845- 878, 2008.

10. Bachschmid, N., Pennacchi, P., Tanzi, E., and Vania, A., Identification of Transverse Crack Position and Depth in Rotor Systems , Meccanica, Vol. 35, No. 1, pp. 563- 582, 2000.

11. Tsai, T.C. and Wang, Y.Z., Vibration Analysis and Diagnosis of a Cracked Shaft , J. Sound and Vibration, Vol. 192, No. 3, pp. 607- 620, 1996.

12. Tsai T.C. and Wang Y.Z., The Vibration of a Multi-crack Rotor , Int. J. Mech. Sciences, Vol. 39, No. 9, pp. 1037-1053, 1997.

13. Haris, C.M. and Crede, C.E., Shock and Vibration Handbook , 2nd Ed., McGraw-Hill, New York, 1976.

14. Shames, H.I. and Dym, C.L., Energy and Finite Element Methods in Structural Mechanics , McGraw-Hill, New York, pp. 200, 1985.

15. Murigendrappa, S.M., Maiti, S.K., and Srirangarajan, H.R., Frequency-based Experimental and Theoretical Identification of Multiple Cracks in Straight Pipes Filled with Fluid , NDT&E Int., Vol. 37, No. 1, pp. 431- 438, 2004.

16. Xiang, J., zhong, Y., Chen, X., and He, Z., Crack Detection in a Shaft by Combination of Wavelet-based Elements and Genetic Algorithm , Int. J. Solids and Structures, Vol. 45, No. 17, pp. 4782-4795, 2008.

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