Adjal yassine

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Transfer matrix method for vibration ana...

Posted: Adjal yassine 25 Product: Maple

November 11 2019

0 0

Program of Transfer matrix method for solving the vibrational behavior of a cracked beam. For more details and comprehension check the paper entitled ''A transfer matrix method for free vibration analysis and crack identification of stepped beams with multiple edge cracks and different boundary conditions ''

MD21 := subs(A[1] = 1, A[2] = 0, A[3] = 0, A[4] = 0, theta11); MD22 := subs(A[1] = 0, A[2] = 1, A[3] = 0, A[4] = 0, theta11); MD23 := subs(A[1] = 0, A[2] = 0, A[3] = 1, A[4] = 0, theta11); MD24 := subs(A[1] = 0, A[2] = 0, A[3] = 0, A[4] = 1, theta11)

TM := Matrix(4, 4, [[MD11, MD12, MD13, MD14], [MD21, MD22, MD23, MD24], [MD31, MD32, MD33, MD34], [MD41, MD42, MD43, MD44]])

Download transfer.mw

Stiffness matrix implementation of a fi...

Posted: Adjal yassine 25

November 07 2019

0 5

MD11 := subs(a[0] = 1, a[1] = 0, a[2] = 0, a[3] = 0, v[i]):

MS11 := subs(a[0] = 0, a[1] = 0, a[2] = 0, a[3] = 0, theta[i]):

MT11 := subs(a[0] = 1, a[1] = 0, a[2] = 0, a[3] = 0, v[j]):

MR11 := subs(a[0] = 1, a[1] = 0, a[2] = 0, a[3] = 0, theta[j]):

$KG := Matrix(4, 4, {(1, 1) = 12*EI/L^3, (1, 2) = 6*EI/L^2, (1, 3) = -12*EI/L^3, (1, 4) = 6*EI/L^2, (2, 1) = 6*EI/L^2, (2, 2) = 4*EI/L, (2, 3) = -6*EI/L^2, (2, 4) = 2*EI/L, (3, 1) = -12*EI/L^3, (3, 2) = -6*EI/L^2, (3, 3) = 12*EI/L^3, (3, 4) = -6*EI/L^2, (4, 1) = 6*EI/L^2, (4, 2) = 2*EI/L, (4, 3) = -6*EI/L^2, (4, 4) = 4*EI/L})$

(1)

Download stiffnesmatrice.mw

Stiffness matrix implementation of a finite element beam based on Euler-Bernoulli theory stiffnesmatrice.mw

Free vibration of a cracked composite be...

Posted: Adjal yassine 25 Product: Maple

November 06 2019

5 0

>	restart: with(LinearAlgebra):

>	# Motion equation ( Vibration of a cracked composite beam using general solution) Edited by Adjal Yassine #

>	####################################################################

Motion equation of flexural vibration in normalized form

>	EIW^(iv)-momega^2*W=0;

(1)

The general solution form of bending vibration equation

>	W1:=A[1]cosh(mux)+A[2]sinh(mux)+A[3]cos(mux)+A[4]sin(mux);

(2)

where

>	E:=2682e6;L:=0.18;h:=0.004;b:=0.02;rho:=2600;area=bh;m:=rhohb;II:=(hb^3)/12:

(3)

>	mu:=((momega^2L^4/EI)^(1/4)):

Expression of cross-sectional rotation , the bending moment shear force and torsional moment are given as follows respectively

>	theta1 := (1/L)(A[1]musinh(mux)+A[2]mucosh(mux)-A[3]musin(mux)+A[4]mucos(mu*x));

(A[1]*mu*sinh(mu*x)+A[2]*mu*cosh(mu*x)-A[3]*mu*sin(mu*x)+A[4]*mu*cos(mu*x))/L

(4)

>	M1:= (EI/L^2)(A[1]mu^2cosh(mux)+A[2]mu^2sinh(mux)-A[3]mu^2cos(mux)-A[4]mu^2sin(mu*x));

EI*(A[1]*mu^2*cosh(mu*x)+A[2]*mu^2*sinh(mu*x)-A[3]*mu^2*cos(mu*x)-A[4]*mu^2*sin(mu*x))/L^2

(5)

>	S1:= (-EI/L^3)(A[1]mu^3sinh(mux)+A[2]mu^3cosh(mux)+A[3]mu^3sin(mux)-A[4]mu^3cos(mu*x));

-EI*(A[1]*mu^3*sinh(mu*x)+A[2]*mu^3*cosh(mu*x)+A[3]*mu^3*sin(mu*x)-A[4]*mu^3*cos(mu*x))/L^3

(6)

>	W2:=A[5]cosh(mux)+A[6]sinh(mux)+A[7]cos(mux)+A[8]sin(mux);

(7)

>	theta2:= (1/L)(A[5]musinh(mux)+A[6]mucosh(mux)-A[7]musin(mux)+A[8]mucos(mu*x));

(A[5]*mu*sinh(mu*x)+A[6]*mu*cosh(mu*x)-A[7]*mu*sin(mu*x)+A[8]*mu*cos(mu*x))/L

(8)

>	M2:= (EI/L^2)(A[5]mu^2cosh(mux)+A[6]mu^2sinh(mux)-A[7]mu^2cos(mux)-A[8]mu^2sin(mu*x));

EI*(A[5]*mu^2*cosh(mu*x)+A[6]*mu^2*sinh(mu*x)-A[7]*mu^2*cos(mu*x)-A[8]*mu^2*sin(mu*x))/L^2

(9)

>	S2:= -(EI/L^3)(A[5]mu^3sinh(mux)+A[6]mu^3cosh(mux)+A[7]mu^3sin(mux)-A[8]mu^3cos(mu*x));

-EI*(A[5]*mu^3*sinh(mu*x)+A[6]*mu^3*cosh(mu*x)+A[7]*mu^3*sin(mu*x)-A[8]*mu^3*cos(mu*x))/L^3

(10)

The boundary conditions at fixed end W1(0)=Theta(0)=0

>	X1:=eval(subs(x=0,W1));

(11)

>	X2:=eval(subs(x=0,theta1));

(mu*A[2]+mu*A[4])/L

(12)

>	X2:=collect(X2,mu)*(L/mu);

(13)

The boundary condtions at free end M2(1)=S2(1)=0

>	X3:=eval(subs(x=1,M2));

EI*(A[5]*mu^2*cosh(mu)+A[6]*mu^2*sinh(mu)-A[7]*mu^2*cos(mu)-A[8]*mu^2*sin(mu))/L^2

(14)

>	X3:=collect(X3,mu)*(L^2/mu^2/EI);

(15)

>	X4:=eval(subs(x=1,S2));

-EI*(A[5]*mu^3*sinh(mu)+A[6]*mu^3*cosh(mu)+A[7]*mu^3*sin(mu)-A[8]*mu^3*cos(mu))/L^3

(16)

>	X4:=collect(X4,mu);

-EI*(cosh(mu)*A[6]+sinh(mu)*A[5]-cos(mu)*A[8]+sin(mu)*A[7])*mu^3/L^3

(17)

>	X4:=collect(X4,EI)*(L^3/mu^3/EI);

(18)

The additional boundary conditions at crack location

>	X5:=combine(M1-M2);

(EI*cosh(mu*x)*mu^2*A[1]-EI*cosh(mu*x)*mu^2*A[5]+EI*sinh(mu*x)*mu^2*A[2]-EI*sinh(mu*x)*mu^2*A[6]-EI*cos(mu*x)*mu^2*A[3]+EI*cos(mu*x)*mu^2*A[7]-EI*sin(mu*x)*mu^2*A[4]+EI*sin(mu*x)*mu^2*A[8])/L^2

(19)

>	X5:=collect(X5,mu);

(EI*cosh(mu*x)*A[1]-EI*cosh(mu*x)*A[5]+EI*sinh(mu*x)*A[2]-EI*sinh(mu*x)*A[6]-cos(mu*x)*EI*A[3]+A[7]*cos(mu*x)*EI-A[4]*sin(mu*x)*EI+A[8]*sin(mu*x)*EI)*mu^2/L^2

(20)

>	X5:=collect(X5,EI)*(L^2/mu^2/EI);

A[1]*cosh(mu*x)-A[5]*cosh(mu*x)+A[2]*sinh(mu*x)-A[6]*sinh(mu*x)-A[3]*cos(mu*x)+A[7]*cos(mu*x)-A[4]*sin(mu*x)+A[8]*sin(mu*x)

(21)

>	X6:=combine(S1-S2);

(-EI*cosh(mu*x)*mu^3*A[2]+EI*cosh(mu*x)*mu^3*A[6]-EI*sinh(mu*x)*mu^3*A[1]+EI*sinh(mu*x)*mu^3*A[5]+EI*cos(mu*x)*mu^3*A[4]-EI*cos(mu*x)*mu^3*A[8]-EI*sin(mu*x)*mu^3*A[3]+EI*sin(mu*x)*mu^3*A[7])/L^3

(22)

>	X6:=collect(X6,mu);

(-EI*cosh(mu*x)*A[2]+EI*cosh(mu*x)*A[6]-EI*sinh(mu*x)*A[1]+EI*A[5]*sinh(mu*x)+cos(mu*x)*A[4]*EI-cos(mu*x)*A[8]*EI-sin(mu*x)*EI*A[3]+sin(mu*x)*A[7]*EI)*mu^3/L^3

(23)

>	X6:=collect(X6,EI)*(L^3/mu^3/EI);

-cosh(mu*x)*A[2]+cosh(mu*x)*A[6]-sinh(mu*x)*A[1]+sinh(mu*x)*A[5]+cos(mu*x)*A[4]-cos(mu*x)*A[8]-sin(mu*x)*A[3]+sin(mu*x)*A[7]

(24)

>	X7:=combine(W2-(W1+c8*S1));

(EI*cosh(mu*x)*c8*mu^3*A[2]+EI*sinh(mu*x)*c8*mu^3*A[1]-EI*cos(mu*x)*c8*mu^3*A[4]+EI*sin(mu*x)*c8*mu^3*A[3]-cosh(mu*x)*A[1]*L^3+cosh(mu*x)*A[5]*L^3-sinh(mu*x)*A[2]*L^3+sinh(mu*x)*A[6]*L^3-cos(mu*x)*A[3]*L^3+cos(mu*x)*A[7]*L^3-sin(mu*x)*A[4]*L^3+sin(mu*x)*A[8]*L^3)/L^3

(25)

>	X8:=combine (theta2-(theta1+c44*M1));

(-EI*cosh(mu*x)*c44*mu^2*A[1]-EI*sinh(mu*x)*c44*mu^2*A[2]+EI*cos(mu*x)*c44*mu^2*A[3]+EI*sin(mu*x)*c44*mu^2*A[4]-L*cosh(mu*x)*mu*A[2]+L*cosh(mu*x)*mu*A[6]-L*sinh(mu*x)*mu*A[1]+L*sinh(mu*x)*mu*A[5]-L*cos(mu*x)*mu*A[4]+L*cos(mu*x)*mu*A[8]+L*sin(mu*x)*mu*A[3]-L*sin(mu*x)*mu*A[7])/L^2

(26)

The characteristic matrix function of frequency

>	FD8:=subs(A[1]=1,A[3]=0,X1);FD12:=subs(A[1]=0,A[3]=0,X1);FD13:=subs(A[1]=0,A[3]=1,X1);FD14:=subs(A[1]=0,A[3]=0,X1);FD15:=subs(A[1]=0,A[3]=0,X1);FD16:=subs(A[1]=0,A[3]=0,X1);FD17:=subs(A[1]=0,A[3]=0,X1);FD18:=subs(A[1]=0,A[3]=0,X1);

(27)

>	FD21:=subs(A[2]=0,A[4]=0,X2);FD22:=subs(A[2]=1,A[4]=0,X2);FD23:=subs(A[2]=0,A[4]=0,X2);FD24:=subs(A[2]=0,A[4]=1,X2);FD25:=subs(A[2]=0,A[4]=0,X2);FD26:=subs(A[2]=0,A[4]=0,X2);FD27:=subs(A[2]=0,A[4]=0,X2);FD28:=subs(A[2]=0,A[4]=0,X2);

(28)

FD31:=subs(A[5]=0,A[6]=0,A[7]=0,A[8]=0,X3);FD32:=subs(A[5]=0,A[6]=0,A[7]=0,A[8]=0,X3);FD33:=subs(A[5]=0,A[6]=0,A[7]=0,A[8]=0,X3);FD34:=subs(A[5]=0,A[6]=0,A[7]=0,A[8]=0,X3);FD35:=subs(A[5]=1,A[6]=0,A[7]=0,A[8]=0,X3);;FD36:=subs(A[5]=0,A[6]=1,A[7]=0,A[8]=0,X3);FD37:=subs(A[5]=0,A[6]=0,A[7]=1,A[8]=0,X3);FD38:=subs(A[5]=0,A[6]=0,A[7]=0,A[8]=1,X3);

(29)

FD41:=subs(A[5]=0,A[6]=0,A[7]=0,A[8]=0,X4);FD42:=subs(A[5]=0,A[6]=0,A[7]=0,A[8]=0,X4);FD43:=subs(A[5]=0,A[6]=0,A[7]=0,A[8]=0,X4);FD44:=subs(A[5]=0,A[6]=0,A[7]=0,A[8]=0,X4);FD45:=subs(A[5]=1,A[6]=0,A[7]=0,A[8]=0,X4);FD46:=subs(A[5]=0,A[6]=1,A[7]=0,A[8]=0,X4);FD47:=subs(A[5]=0,A[6]=0,A[7]=1,A[8]=0,X4);FD48:=subs(A[5]=0,A[6]=0,A[7]=0,A[8]=1,X4);

(30)

FD51:=subs(A[1]=1,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X5);FD52:=subs(A[1]=0,A[2]=1,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X5);FD53:=subs(A[1]=0,A[2]=0,A[3]=1,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X5);FD54:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=1,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X5);FD55:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=1,A[6]=0,A[7]=0,A[8]=0,X5);FD56:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=1,A[7]=0,A[8]=0,X5);FD57:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=1,A[8]=0,X5);FD58:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=1,X5);

(31)

FD61:=subs(A[1]=1,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X6);FD62:=subs(A[1]=0,A[2]=1,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X6);FD63:=subs(A[1]=0,A[2]=0,A[3]=1,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X6);FD64:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=1,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X6);FD65:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=1,A[6]=0,A[7]=0,A[8]=0,X6);FD66:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=1,A[7]=0,A[8]=0,X6);FD67:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=1,A[8]=0,X6);FD68:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=1,X6);

(32)

FD71:=subs(A[1]=1,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X7);FD72:=subs(A[1]=0,A[2]=1,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X7);FD73:=subs(A[1]=0,A[2]=0,A[3]=1,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X7);FD74:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=1,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X7);FD75:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=1,A[6]=0,A[7]=0,A[8]=0,X7);FD76:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=1,A[7]=0,A[8]=0,X7);FD77:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=1,A[8]=0,X7);FD78:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=1,X7);

(EI*sinh(mu*x)*c8*mu^3-cosh(mu*x)*L^3)/L^3

(EI*cosh(mu*x)*c8*mu^3-sinh(mu*x)*L^3)/L^3

(EI*sin(mu*x)*c8*mu^3-L^3*cos(mu*x))/L^3

(-EI*cos(mu*x)*c8*mu^3-sin(mu*x)*L^3)/L^3

(33)

FD81:=subs(A[1]=1,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X8);FD82:=subs(A[1]=0,A[2]=1,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X8);FD83:=subs(A[1]=0,A[2]=0,A[3]=1,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X8);FD84:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=1,A[5]=0,A[6]=0,A[7]=0,A[8]=0,X8);FD85:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=1,A[6]=0,A[7]=0,A[8]=0,X8);FD86:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=1,A[7]=0,A[8]=0,X8);FD87:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=1,A[8]=0,X8);FD88:=subs(A[1]=0,A[2]=0,A[3]=0,A[4]=0,A[5]=0,A[6]=0,A[7]=0,A[8]=1,X8);

(-EI*cosh(mu*x)*c44*mu^2-L*sinh(mu*x)*mu)/L^2

(-EI*sinh(mu*x)*c44*mu^2-L*cosh(mu*x)*mu)/L^2

(EI*cos(mu*x)*c44*mu^2+L*sin(mu*x)*mu)/L^2

(EI*sin(mu*x)*c44*mu^2-L*cos(mu*x)*mu)/L^2

(34)

MM:=matrix(8,8,[[FD11,FD12,FD13,FD14,FD15,FD16,FD17,FD18],[FD21,FD22,FD23,FD24,FD25,FD26,FD27,FD28],[FD31,FD32,FD33,FD34,FD35,FD36,FD37,FD38],[FD41,FD42,FD43,FD44,FD45,FD46,FD47,FD48],[FD51,FD52,FD53,FD54,FD55,FD56,FD57,FD58],[FD61,FD62,FD63,FD64,FD65,FD66,FD67,FD68],[FD71,FD72,FD73,FD74,FD75,FD76,FD77,FD78],[FD81,FD82,FD83,FD84,FD85,FD86,FD87,FD88]]);

$MM := Matrix(8, 8, {(1, 1) = FD11, (1, 2) = 0, (1, 3) = 1, (1, 4) = 0, (1, 5) = 0, (1, 6) = 0, (1, 7) = 0, (1, 8) = 0, (2, 1) = 0, (2, 2) = 1, (2, 3) = 0, (2, 4) = 1, (2, 5) = 0, (2, 6) = 0, (2, 7) = 0, (2, 8) = 0, (3, 1) = 0, (3, 2) = 0, (3, 3) = 0, (3, 4) = 0, (3, 5) = cosh(mu), (3, 6) = sinh(mu), (3, 7) = -cos(mu), (3, 8) = -sin(mu), (4, 1) = 0, (4, 2) = 0, (4, 3) = 0, (4, 4) = 0, (4, 5) = -sinh(mu), (4, 6) = -cosh(mu), (4, 7) = -sin(mu), (4, 8) = cos(mu), (5, 1) = cosh(mu*x), (5, 2) = sinh(mu*x), (5, 3) = -cos(mu*x), (5, 4) = -sin(mu*x), (5, 5) = -cosh(mu*x), (5, 6) = -sinh(mu*x), (5, 7) = cos(mu*x), (5, 8) = sin(mu*x), (6, 1) = -sinh(mu*x), (6, 2) = -cosh(mu*x), (6, 3) = -sin(mu*x), (6, 4) = cos(mu*x), (6, 5) = sinh(mu*x), (6, 6) = cosh(mu*x), (6, 7) = sin(mu*x), (6, 8) = -cos(mu*x), (7, 1) = (EI*sinh(mu*x)*c8*mu^3-cosh(mu*x)*L^3)/L^3, (7, 2) = (EI*cosh(mu*x)*c8*mu^3-sinh(mu*x)*L^3)/L^3, (7, 3) = (EI*sin(mu*x)*c8*mu^3-L^3*cos(mu*x))/L^3, (7, 4) = (-EI*cos(mu*x)*c8*mu^3-sin(mu*x)*L^3)/L^3, (7, 5) = cosh(mu*x), (7, 6) = sinh(mu*x), (7, 7) = cos(mu*x), (7, 8) = sin(mu*x), (8, 1) = (-EI*cosh(mu*x)*c44*mu^2-L*sinh(mu*x)*mu)/L^2, (8, 2) = (-EI*sinh(mu*x)*c44*mu^2-L*cosh(mu*x)*mu)/L^2, (8, 3) = (EI*cos(mu*x)*c44*mu^2+L*sin(mu*x)*mu)/L^2, (8, 4) = (EI*sin(mu*x)*c44*mu^2-L*cos(mu*x)*mu)/L^2, (8, 5) = sinh(mu*x)*mu/L, (8, 6) = cosh(mu*x)*mu/L, (8, 7) = -sin(mu*x)*mu/L, (8, 8) = cos(mu*x)*mu/L})$

(35)

Program end

Download Vibration_of_a_cracked_composite_beam.mw

>	restart: with(LinearAlgebra):

>	# Motion equation ( Vibration of a cracked composite beam using general solution) Edited by Adjal Yassine #

>	####################################################################