calculo estructural final.docx

7/23/2019 CALCULO ESTRUCTURAL FINAL.docx

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Minera del Norte S.A. Proyecto Anubia Proyecto: Diseo de la planta de Lixiviacin y lotacin para !inerales de cobre"

#alculo $structural Autodes% &obot Structural" Pg. 1

CALCULO ESTRUCTURAL

CONTENIDO

'. M$M(&)A D$ #AL#*L(S.....................................................................3

'.'. (+,$-)(S.........................................................................................3

'./. #(NS)D$&A#)(N$S............................................................................3

'.0. P&(P)$DAD$S M$#AN)#AS D$L A#$&( A01.......................................4

'.2. $S-*D)( D$ #A&3AS.........................................................................4'.4. #A&3AS M*$&-AS.............................................................................4

'.1. #A&3AS )AS...................................................................................5

'.5. #A&3AS D$ )$N-(............................................................................5

'.6. #A&3A S)SM)#A..................................................................................7

'.7. #(M+)NA#)(N D$ #A&3AS.................................................................8

/. $S-&*#-*&A $N #(N,*N-(..............................................................9

0. $S-&*#-*&A D$ S(P(&-$ PA&A 3&)SL8...........................................9

0.'. 3$(M$-&)A D$ LA $S-&*#-*&A S(P(&-$ D$ 3&)SL8......................9

0./. MAPA D$ #(L(&$S...........................................................................10

0.0. D)A3&AMA D$ $S*$&9(S $N &$3)(N$S #&-)#AS........................11

0.2. &$S*L-AD(S....................................................................................11

0.4. &$A##)(N$S....................................................................................33

0.1. #(N#L*#)(N$S...............................................................................34

2. $S-&*#-*&A D$ S(P(&-$ D$ -(LA..............................................34

2.'. 3$(M$-&)A D$ LA $S-&*#-*&A D$ -(LA......................................342./. MAPA D$ #(L(&$S...........................................................................35

2.0. D)A3&AMA D$ $S*$&9(S $N &$3)(N$S #&-)#AS........................35

2.2. &$S*L-AD(S....................................................................................36

2.4. &$A##)(N$S....................................................................................44

2.1. #(N#L*#)(N$S...............................................................................44

4. $S-&*#-*&A PA&A A#$S( '............................................................45

4.'. 3$(M$-&)A PA&A $S-&*#-*&AS D$ A##$S( '...............................45

4./. MAPA D$ #(L(&$S...........................................................................45

Calle Jorge Polar 107 Urb. La Victoria Arequipa Per Telefax 0!"#$%$0!1 &P'()$7$!1 ***.co+,orcio,-c.co&PC /!%1/0$/ 23T2L )14!0!"
http://www.consorciosyc.com/http://www.consorciosyc.com/


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#alculo $structural Autodes% &obot Structural" Pg. $

4.0. D)A3&AMA D$ $S*$&9(S $N &$3)(N$S #&-)#AS........................46

4.2. &$S*L-AD(S....................................................................................46

4.4. &$A##)(N$S....................................................................................68

4.1. #(N#L*#)(N$S...............................................................................68

1. $S-&*#-*&A PA&A A#$S( / ............................................................69

1.'. 3$(M$-&)A PA&A $S-&*#-*&AS D$ A##$S( /...............................69

1./. MAPA D$ #(L(&$S...........................................................................69

1.0. D)A3&AMA D$ $S*$&9(S $N &$3)(N$S #&-)#AS........................70

1.2. &$S*L-AD(S....................................................................................70

1.4. &$A##)(N$S..................................................................................111

1.1. #(N#L*#)(N$S.............................................................................1115. $S-&*#-*&A PA&A A,A N;'..........................................................113

5.'. 3$(M$-&)A PA&A $S-&*#-*&A D$ A,A N;'.................................113

5./. MAPA D$ #(L(&$S.........................................................................113

5.0. D)A3&AMA D$ $S*$&9(S $N &$3)(N$S #&-)#AS......................114

5.2. &$S*L-AD(S..................................................................................114

5.4. &$A##)(N$S..................................................................................220

5.1. #(N#L*#)(N$S.............................................................................220

'. M$M(&)A D$ #AL#*L(S



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#alculo $structural Autodes% &obot Structural" Pg.

La presente informacin nos mostrara la forma con la cual ha sidocalculado las estructuras en acero y en concreto armado.mponiendo desde la !ases de resistencia de materiales las formulasy procedimientos esta!lecidos por L"#$ y por las normas peruanas

%&'( dando como resultado conclusiones satisfactorias y se)uraspara la seleccin apropiada de materiales.

'.'. (+,$-)(S

*propiada seleccin de materiales Lista de materiales +so correcto de las %ormas &,cnicas 'eruanas *plicacin del m,todo de se)undo orden '-delta para la

resolucin de las estructuras hiperestticas *plicacin del /,todo de lementos #initos. +so apropiado de softare 5Auto6e, &obot 8tructural

Profe,,io+al9 aluacin por ratios para las conclusiones

'./. #(NS)D$&A#)(N$S

Los criterios de calculo estn re)idos por las normas internacionalesde L&D Speci'777"

Los clculos fueron realiados por el pro)rama *utodes "o!ottructural analysis 'rofessional 2015

Los materiales son de acero estructural *36

La estructura ha sido estudiada en la u!icacin urahuasi proinciade *!ancay( departamento de *purmac a una altitud de 2300- 4350msnm.



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#alculo $structural Autodes% &obot Structural" Pg. "

'.0. P&(P)$DAD$S M$#AN)#AS D$L A#$&( A01

'.2. $S-*D)( D$ #A&3AS

l estudio de la car)as son imprescindi!les ya :ue por su naturaleaestas afectan a las estructuras el cual el n)eniero calculista estproisto al tener en cuenta en su desarrollo de su clculo. &anto lascar)as actias como las reactias sern las si)uientes;

ar)as muertas ar)as ias ar)as de iento ar)as ssmicas

'.4. #A&3AS M*$&-AS

on car)as reactias el cual proienen de su propio peso

'.1. #A&3AS )AS

stas pueden ser puntuales como distri!uidas en toda una super


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#alculo $structural Autodes% &obot Structural" Pg. !

=h?=elocidad de dise>o en la altura de h en m@hr

=? =elocidad de dise>o hasta 10 m

h? *ltura so!re el terreno en metros

ar)a eAterior de iento

Ph=0.005CVh2

'h; 'resin o succin eBercida por el iento a una altura h en C)f@m2

; factor de forma adimensional indicado en la ta!la 4

=h?=elocidad de dise>o en la altura de h en m@hr de


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#alculo $structural Autodes% &obot Structural" Pg. )



7/221



'.6. #A&3A S)SM)#A

ar)a :ue por su naturalea es producida por los sismos y posi!lesterremotos :ue se puedan presentar en un futuro.



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#alculo $structural Autodes% &obot Structural" Pg. %

'.7. #(M+)NA#)(N D$ #A&3AS

sta com!inacin est dispuesta por la 090 D1.4 F 2E

P=1.6Cl+1.2Cd+0.8CW

Cl ? car)a ia

Cd ? car)a muerta

CW ? car)a de iento



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#alculo $structural Autodes% &obot Structural" Pg. /

/. $S-&*#-*&A $N #(N,*N-(

0. $S-&*#-*&A D$ S(P(&-$ PA&A 3&)SL8

0.'. 3$(M$-&)A D$ LA $S-&*#-*&A S(P(&-$ D$ 3&)SL8



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0./. MAPA D$ #(L(&$S



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0.0. D)A3&AMA D$ $S*$&9(S $N &$3)(N$S #&-)#AS

0.2. &$S*L-AD(S

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------

CODE: L&D Speci'777ANALYSIS TYPE: Member Verification

-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: 2 Column_2 POINT: 3 COORDINATE: x = !"" L =

#""!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:

Governing Load Case: $ C%M&IN'CI%N (!2")2(!*")3("!#"

-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION PARAMETERS: W 12x300=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:



12/221


#alculo $structural Autodes% &obot Structural" Pg. 1$

L, = #""!""""" mm 8L,/r, = 3!*2 Lb = #""!""""" mm

L = #""!""""" mm 8L/r = 1*!*3 Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------

INTERNAL FORCES: NOMINAL STRENGTHS:

9u = "13*!#433 .f 9n = 3*"22!##2 .fMu, = -1##1!3*4 .f(mm Vu, = *"!*$241 .f Mn, =

4"#$$"3!3$14 .f(mm Vn, = $1"$!2#313 .f

Mu = -2#4$!24#3# .f(mm Vu = -2!42#$ .f Mn =

12333$"!*2#* .f(mm Vn = 331$2!"4$ .f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!$ ? !"" L@+D A-&>

Vu,/+i:(Vn,> = "!"" ? !"" Vu/+i:(Vn> = "!" ? !"" L@+D +2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS

Deflections Not analyzed

Displacements

:x = " mm ? :x max = L/$"!"" = 2 mm Verifie0

Governing Load Case: 2 C'@G' VIV'

:, = " mm ? :, max = L/$"!"" = 2 mm Verifie0


-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


----------------------------------------------------------------------------------------------------------------------------------------

CODE GROUP:

MEMBER: 3 Column_3 POINT: COORDINATE: x = "!"" L =

"!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------



13/221



SECTION PARAMETERS: W 12x30

0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = #""!""""" mm 8L,/r, = 3!*2

L = #""!""""" mm 8L/r = 1*!*3

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = 2*2"!1$"$4 .f 9n = 3*"22!##2 .f

Vu, = !$3* .f Vn, = $1"$!2#313.f

Vu = -33!2*""2 .f Vn = 331$2!"4$

.f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Non-com = "! ? !"" L@+D E2->

Vu,/+i:(Vn,> = "!"" ? !"" Vu/+i:(Vn> = "!"" ? !"" L@+D +2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS


Displacements





-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------

---------CODE GROUP:



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#alculo $structural Autodes% &obot Structural" Pg. 1"


#""!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:

Governing Load Case: $ C%M&IN'CI%N (!2")2(!*")3("!#"-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = #""!""""" mm 8L,/r, = 3!*2 Lb = #""!""""" mm

L = #""!""""" mm 8L/r = 1*!*3 Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = *331!#3# .f 9n = 3*"22!##2 .f

Mu, = -3"*2!$$*#3 .f(mm Vu, = *!$14## .f Mn, =

4"#$$"3!3$14 .f(mm Vn, = $1"$!2#313 .fMu = -24"#4!#4"$ .f(mm Vu = -"!1242" .f Mn =

12333$"!*2#* .f(mm Vn = 331$2!"4$ .f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!* ? !"" L@+D A-&>

Vu,/+i:(Vn,> = "!"" ? !"" Vu/+i:(Vn> = "!" ? !"" L@+D +2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS


Displacements





-------------------------------------------------------------------------------------------------------------------------------



15/221


#alculo $structural Autodes% &obot Structural" Pg. 1!

---------

Section OK !!!

STEEL DESIGN----------------------------------------------------------------------------------------------------------------------------------------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: $ Column_$ POINT: 3 COORDINATE: x = !"" L =

#""!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


----------------------------------------------------------------------------------------------------------------------------------------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = #""!""""" mm 8L,/r, = 3!*2 Lb = #""!""""" mm

L = #""!""""" mm 8L/r = 1*!*3 Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = "2!4242 .f 9n = 3*"22!##2 .f

Mu, = 2"$22$!"*213 .f(mm Vu, = "!1 .f Mn, =

4"#$$"3!3$14 .f(mm Vn, = $1"$!2#313 .f

Mu = -#1#!"4" .f(mm Vu = **4!$*41# .f Mn =12333$"!*2#* .f(mm Vn = 331$2!"4$ .f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!" ? !"" L@+D A-&>Vu,/+i:(Vn,> = "!"" ? !"" Vu/+i:(Vn> = "!"2 ? !"" L@+D +2-2>



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#alculo $structural Autodes% &obot Structural" Pg. 1)

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS


Displacements





-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------CODE: L&D Speci'777ANALYSIS TYPE: Member Verification

-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: * &eam_* POINT: COORDINATE: x = "!"" L =

"!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = $#!""""" mm 8L,/r, = $!1

L = $#!""""" mm 8L/r = 4!*1

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = 41!*#1 .f 9n = $3213!3"3## .f

Vu, = -"!2*2$ .f Vn, = $1"$!2#313

.f

Vu = 212$!$134* .f Vn = 331$2!"4$

.f-------------------------------------------------------------------------------------------------------------------------------



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---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Non-com = "!"" ? !"" L@+D E2->

Vu,/+i:(Vn,> = "!"" ? !"" Vu/+i:(Vn> = "!"# ? !"" L@+D +2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS

Deflections

u, = " mm ? u, max = L/2""!"" = 1 mm Verifie0


u = " mm ? u max = L/2""!"" = 1 mm Verifie0


Displacements Not analyzed

-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: &eam_ POINT: 3 COORDINATE: x = !"" L =

3**!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

----------------------------------------------------------------------------------------------------------------------------------------



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#alculo $structural Autodes% &obot Structural" Pg. 1%

MEMBER PARAMETERS:

L, = 3**!""""" mm 8L,/r, = "!31 Lb = 3**!""""" mm

L = 3**!""""" mm 8L/r = 3$!34 Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------


Mux = -"4!221*$ .f(mm fu:,Bmx = *!13$ .f/cm2

9u = 1*$!##"2* .f fu:Bmx = 3!##$3 .f/cm2 9n = $3213!3"3##

.f

Mu, = -1#$31*!1*$1 .f(mm Vu, = -"!3#$13 .f Mn, =

4"#$$"3!3$14 .f(mm Vn, = $1"$!2#313 .f

Mu = 1*#!$444 .f(mm Vu = -*2**!13*$3 .f Mn = 12333$"!*2#* .f(mm Vn =

331$2!"4$ .f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!"4 ? !"" L@+D A-&>

Vu,/+i:(Vn,> ) fu:,Bmx/"!*(+i:(+,> = "!"" ? !"" Vu/+i:(Vn> ) fu:Bmx/"!*(+i:(+,> = "!2 ?

!"" L@+D +2-2> A2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS

Deflections

u, = " mm ? u, max = L/2""!"" = mm Verifie0


u = " mm ? u max = L/2""!"" = mm Verifie0



-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN----------------------------------------------------------------------------------------------------------------------------------------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: # &eam_# POINT: COORDINATE: x = "!"" L =

"!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------



19/221


20/221


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#alculo $structural Autodes% &obot Structural" Pg. $1

LIMIT DISPLACEMENTS

Deflections



u = " mm ? u max = L/2""!"" = 4 mm Verifie0Governing Load Case: 2 C'@G' VIV'


-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------

CODE: L&D Speci'777

ANALYSIS TYPE: Member Verification-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: " Column_" POINT: 3 COORDINATE: x = !"" L =

#""!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2-------------------------------------------------------------------------------------------------------------------------------

---------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------MEMBER PARAMETERS:

L, = #""!""""" mm 8L,/r, = 3!*2 Lb = #""!""""" mm

L = #""!""""" mm 8L/r = 1*!*3 Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = "13*!#433 .f 9n = 3*"22!##2 .f

Mu, = -1##1!3*4 .f(mm Vu, = -*"!*$241 .f Mn, =

4"#$$"3!3$14 .f(mm Vn, = $1"$!2#313 .f

Mu = 2#4$!24#3# .f(mm Vu = -2!42#$ .f Mn =

12333$"!*2#* .f(mm Vn = 331$2!"4$ .f

-------------------------------------------------------------------------------------------------------------------------------

---------COEFFICIENTS:



22/221


#alculo $structural Autodes% &obot Structural" Pg. $$

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!$ ? !"" L@+D A-&>

Vu,/+i:(Vn,> = "!"" ? !"" Vu/+i:(Vn> = "!" ? !"" L@+D +2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS


Displacements


Governing Load Case: 2 C'@G' VIV':, = " mm ? :, max = L/$"!"" = 2 mm Verifie0


-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


----------------------------------------------------------------------------------------------------------------------------------------

CODE GROUP:

MEMBER: Column_ POINT: COORDINATE: x = "!"" L =

"!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

----------------------------------------------------------------------------------------------------------------------------------------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = #""!""""" mm 8L,/r, = 3!*2



23/221



L = #""!""""" mm 8L/r = 1*!*3

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = 2*2"!1$"$4 .f 9n = 3*"22!##2 .f

Vu, = -!$3* .f Vn, = $1"$!2#313.f

Vu = -33!2*""2 .f Vn = 331$2!"4$

.f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Non-com = "! ? !"" L@+D E2->

Vu,/+i:(Vn,> = "!"" ? !"" Vu/+i:(Vn> = "!"" ? !"" L@+D +2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS


Displacements





-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------



#""!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------



24/221


#alculo $structural Autodes% &obot Structural" Pg. $"


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = #""!""""" mm 8L,/r, = 3!*2 Lb = #""!""""" mm

L = #""!""""" mm 8L/r = 1*!*3 Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = *331!#3# .f 9n = 3*"22!##2 .f

Mu, = -3"*2!$$*#3 .f(mm Vu, = -*!$14## .f Mn, =4"#$$"3!3$14 .f(mm Vn, = $1"$!2#313 .f

Mu = 24"#4!#4"$ .f(mm Vu = -"!1242" .f Mn =

12333$"!*2#* .f(mm Vn = 331$2!"4$ .f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!* ? !"" L@+D A-&>

Vu,/+i:(Vn,> = "!"" ? !"" Vu/+i:(Vn> = "!" ? !"" L@+D +2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS


Displacements





-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------




25/221


#alculo $structural Autodes% &obot Structural" Pg. $!


#""!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = #""!""""" mm 8L,/r, = 3!*2 Lb = #""!""""" mm

L = #""!""""" mm 8L/r = 1*!*3 Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = "2!4242 .f 9n = 3*"22!##2 .f

Mu, = 2"$22$!"*213 .f(mm Vu, = -"!1 .f Mn, =

4"#$$"3!3$14 .f(mm Vn, = $1"$!2#313 .fMu = #1#!"4" .f(mm Vu = **4!$*41# .f Mn = 12333$"!*2#* .f(mm Vn =

331$2!"4$ .f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!" ? !"" L@+D A-&>

Vu,/+i:(Vn,> = "!"" ? !"" Vu/+i:(Vn> = "!"2 ? !"" L@+D +2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS


Displacements





-------------------------------------------------------------------------------------------------------------------------------



26/221


#alculo $structural Autodes% &obot Structural" Pg. $)

---------

Section OK !!!

STEEL DESIGN----------------------------------------------------------------------------------------------------------------------------------------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: 1 &eam_1 POINT: COORDINATE: x = "!"" L =

"!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


----------------------------------------------------------------------------------------------------------------------------------------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = $#!""""" mm 8L,/r, = $!1

L = $#!""""" mm 8L/r = 4!*1

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = 41!*#1 .f 9n = $3213!3"3## .f

Vu, = "!2*2$ .f Vn, = $1"$!2#313

.f

Vu = 212$!$134* .f Vn = 331$2!"4$.f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Non-com = "!"" ? !"" L@+D E2->Vu,/+i:(Vn,> = "!"" ? !"" Vu/+i:(Vn> = "!"# ? !"" L@+D +2-2>



27/221


#alculo $structural Autodes% &obot Structural" Pg. $7

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS

Deflections

u, = " mm ? u, max = L/2""!"" = 1 mm Verifie0Governing Load Case: 2 C'@G' VIV'




-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: $ &eam_$ POINT: 3 COORDINATE: x = !"" L =

3**!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = 3**!""""" mm 8L,/r, = "!31 Lb = 3**!""""" mm

L = 3**!""""" mm 8L/r = 3$!34 Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------


Mux = "4!221*$ .f(mm fu:,Bmx = *!13$ .f/cm2

9u = 1*$!##"2* .f fu:Bmx = 3!##$3 .f/cm2 9n = $3213!3"3##

.f

Mu, = -1#$31*!1*$1 .f(mm Vu, = "!3#$13 .f Mn, =

4"#$$"3!3$14 .f(mm Vn, = $1"$!2#313 .fMu = -1*#!$444 .f(mm Vu = -*2**!13*$3 .f Mn =



28/221


#alculo $structural Autodes% &obot Structural" Pg. $%

12333$"!*2#* .f(mm Vn = 331$2!"4$ .f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

----------------------------------------------------------------------------------------------------------------------------------------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!"4 ? !"" L@+D A-&>


!"" L@+D +2-2> A2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS

Deflections

u, = " mm ? u, max = L/2""!"" = mm Verifie0


u = " mm ? u max = L/2""!"" = mm Verifie0



-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: * &eam_* POINT: COORDINATE: x = "!"" L =

"!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION PARAMETERS: W 12x300=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3



29/221


#alculo $structural Autodes% &obot Structural" Pg. $/

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = $2!""""" mm 8L,/r, = !$ Lb = $2!""""" mm

L = $2!""""" mm 8L/r = 34!1" Cb = !""-------------------------------------------------------------------------------------------------------------------------------

---------


Mux = -4#$!$11* .f(mm fu:,Bmx = $!4"11 .f/cm2

9u = 144!1"2# .f fu:Bmx = 3!12*2 .f/cm2 9n = $3213!3"3##

.f

Mu, = -$1$21!$"*2" .f(mm Vu, = -"!*#33 .f Mn, =

4"#$$"3!3$14 .f(mm Vn, = $1"$!2#313 .f

Mu = -1*#!$444 .f(mm Vu = *214!#"**1 .f Mn =

12333$"!*2#* .f(mm Vn = 331$2!"4$ .f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!"4 ? !"" L@+D A-&>


!"" L@+D +2-2> A2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS

Deflections

u, = " mm ? u, max = L/2""!"" = # mm Verifie0


u = " mm ? u max = L/2""!"" = # mm Verifie0



-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: &eam_ POINT: 3 COORDINATE: x = !"" L =

"!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:



30/221




-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

----------------------------------------------------------------------------------------------------------------------------------------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = "!""""" mm 8L,/r, = 3!34 Lb = "!""""" mm

L = "!""""" mm 8L/r = 1$!#$ Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------


Mux = #1#!"4" .f(mm fu:,Bmx = 1!4#2#4 .f/cm2

9u = **4!$*41# .f fu:Bmx = 2!41113 .f/cm2 9n = $3213!3"3##

.f

Mu, = -2"$22$!"*212 .f(mm Vu, = "!1 .f Mn, =

4"#$$"3!3$14 .f(mm Vn, = $1"$!2#313 .f

Vu = -"2!4242 .f Vn = 331$2!"4$

.f

----------------------------------------------------------------------------------------------------------------------------------------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com = "!" ? !"" L@+D A-&>


!"" L@+D +2-2> A2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS

Deflections






-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!



31/221



STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: # &eam_# POINT: COORDINATE: x = "!"" L =

"!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

----------------------------------------------------------------------------------------------------------------------------------------

MEMBER PARAMETERS:

L, = ""!""""" mm 8L,/r, = 2!#* Lb = ""!""""" mm

L = ""!""""" mm 8L/r = 11!"1 Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = *2!#43# .f 9n = $3213!3"3## .f

Mu, = -242*23!13"3 .f(mm Mn, =

4"#$$"3!3$14 .f(mm

Mu = 33!431" .f(mm Vu = *3$!1$4"* .f Mn = 12333$"!*2#* .f(mm Vn =

331$2!"4$ .f

----------------------------------------------------------------------------------------------------------------------------------------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!"2 ? !"" L@+D A-&>

Vu/+i:(Vn> = "!2$ ? !"" L@+D +2-2>

----------------------------------------------------------------------------------------------------------------------------------------



32/221



LIMIT DISPLACEMENTS

Deflections



u = " mm ? u max = L/2""!"" = 4 mm Verifie0Governing Load Case: 2 C'@G' VIV'


-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------

CODE: L&D Speci'777


---------

CODE GROUP:

MEMBER: 4 &eam_4 POINT: 3 COORDINATE: x = !"" L =

""!""""" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2-------------------------------------------------------------------------------------------------------------------------------

---------


0=32!12""" mm ',=3"!*""2 mm2 '=2"*3!22*# mm2 'x=$*"!4$*1"

mm2

b=*$!*"#"" mm I,=44"*3"4!242#" mm1 I=#11414!434*# mm1 5=4"2!*$"

mm1

t6=*!*"1"" mm S,=*31**!"$34# mm3 S="2"12!1*44 mm3

tf=!*"" mm 7,="*2#2!1$#1" mm3 7=$***"!33#1 mm3

-------------------------------------------------------------------------------------------------------------------------------

---------MEMBER PARAMETERS:

L, = ""!""""" mm 8L,/r, = 2!#* Lb = ""!""""" mm

L = ""!""""" mm 8L/r = 11!"1 Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------


9u = *"!$#* .f 9n = $3213!3"3## .f

Mu, = -24"2**!$23"3 .f(mm Mn, =

4"#$$"3!3$14 .f(mm

Mu = 2$*!##"" .f(mm Vu = -$4!"23"* .f Mn = 12333$"!*2#* .f(mm Vn =

331$2!"4$ .f

-------------------------------------------------------------------------------------------------------------------------------

---------COEFFICIENTS:



33/221


#alculo $structural Autodes% &obot Structural" Pg.

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!"2 ? !"" L@+D A-&>

Vu/+i:(Vn> = "!2$ ? !"" L@+D +2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS

Deflections






-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

0.4. &$A##)(N$S



34/221



0.1. #(N#L*#)(N$S

La estructura fue ealuada por #/ Dm,todo de elementos


35/221


#alculo $structural Autodes% &obot Structural" Pg. !

2.0. D)A3&AMA D$ $S*$&9(S $N &$3)(N$S #&-)#AS

2.2. &$S*L-AD(S

STEEL DESIGN



36/221


37/221



STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------

CODE: L&D Speci'777


---------

CODE GROUP:

MEMBER: 1 Sim


38/221


#alculo $structural Autodes% &obot Structural" Pg. %

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: $ Sim


39/221


#alculo $structural Autodes% &obot Structural" Pg. /

-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN----------------------------------------------------------------------------------------------------------------------------------------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: * Sim



40/221


#alculo $structural Autodes% &obot Structural" Pg. "0

Vu,/+i:(Vn,> ) fu:,Bmx/"!*(+i:(+,> = "!" ? !"" Vu/+i:(Vn> ) fu:Bmx/"!*(+i:(+,> = "!" ?

!"" L@+D +2-2> A2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: Sim


41/221


42/221


#alculo $structural Autodes% &obot Structural" Pg. "$

-------------------------------------------------------------------------------------------------------------------------------

---------

VERIFICATION FORMULAS:

9u/+ic(9n> ) #/4(Mu,/+ib(Mn,> ) Mu/+ib(Mn>> = "!$3 ? !"" L@+D A-'>

Vu,/+i:(Vn,> ) fu:,Bmx/"!*(+i:(+,> = "!"" ? !"" Vu/+i:(Vn> ) fu:Bmx/"!*(+i:(+,> = "!"2 ?

!"" L@+D +2-2> A2-2>-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:MEMBER: 4 Sim


43/221



-------------------------------------------------------------------------------------------------------------------------------

---------


9u/2(+ic(9n> ) Mu,/+ib(Mn,> ) Mu/+ib(Mn>> = "!2 ? !"" L@+D A-&>

-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:

MEMBER: " Sim


44/221


#alculo $structural Autodes% &obot Structural" Pg. ""


9u/2(+it(9n> ) Mu,/+ib(Mn,> ) Mu/+ib(Mn>> = "!$# ? !"" L@+D A-&>

-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

2.4. &$A##)(N$S

2.1. #(N#L*#)(N$S

La estructura fue ealuada por #/ Dm,todo de elementos


45/221


#alculo $structural Autodes% &obot Structural" Pg. "!

4.'. 3$(M$-&)A PA&A $S-&*#-*&AS D$ A##$S( '

4./. MAPA D$ #(L(&$S

4.0. D)A3&AMA D$ $S*$&9(S $N &$3)(N$S #&-)#AS



46/221


#alculo $structural Autodes% &obot Structural" Pg. ")

4.2. &$S*L-AD(S

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:MEMBER: In POINT: 3 COORDINATE: x = !"" L ="2"!"" mm

-------------------------------------------------------------------------------------------------------------------------------

---------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION PARAMETERS: C 6x10.5

0=$2 mm ',=#4# mm2 '=2$ mm2 'x=4# mm2

b=$2 mm I,=*2#$"4$ mm1 I=3$4$4 mm1 5=$32# mm1

t6=# mm S,=#21#2 mm3 S=42 mm3

tf=4 mm 7,="22 mm3 7=#*# mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = "2"!"" mm 8L,/r, = #! Lb = "2"!"" mm

L = "2"!"" mm 8L/r = $!# Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------INTERNAL FORCES: NOMINAL STRENGTHS:



47/221


#alculo $structural Autodes% &obot Structural" Pg. "7

9u = 2432!43$4$ .f 9n = 34"3*!#4#3 .f

Mu, = -41*3!"413 .f(mm Vu, = *4!1*1 .f Mn, =

2$44#4*!$#"3 .f(mm Vn, = 3"!*32 .f

Mu = -2#$*!#2344 .f(mm Vu = -4"!4$ .f Mn =

$"1#3!#3 .f(mm Vn = 4"!431# .f

----------------------------------------------------------------------------------------------------------------------------------------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

-------------------------------------------------------------------------------------------------------------------------------

---------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!$ ? !"" L@+D A-&>

Vu,/+i:(Vn,> = "!" ? !"" Vu/+i:(Vn> = "!" ? !"" L@+D +2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS


Displacements

:x = " mm ? :x max = L/$"!"" = mm Verifie0

Governing Load Case: 2 C'@C' VIV'

:, = " mm ? :, max = L/$"!"" = mm Verifie0


-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------

---------


-------------------------------------------------------------------------------------------------------------------------------

---------

CODE GROUP:


"2"!"" mm

----------------------------------------------------------------------------------------------------------------------------------------

LOADS:


-------------------------------------------------------------------------------------------------------------------------------

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------


0=$2 mm ',=#4# mm2 '=2$ mm2 'x=4# mm2b=$2 mm I,=*2#$"4$ mm1 I=3$4$4 mm1 5=$32# mm1



48/221


49/221


#alculo $structural Autodes% &obot Structural" Pg. "/

---------

MATERIAL:

STEEL +, = 2$3"!" .f/cm2

-------------------------------------------------------------------------------------------------------------------------------

---------


0=$2 mm ',=#4# mm2 '=2$ mm2 'x=4# mm2

b=$2 mm I,=*2#$"4$ mm1 I=3$4$4 mm1 5=$32# mm1

t6=# mm S,=#21#2 mm3 S=42 mm3

tf=4 mm 7,="22 mm3 7=#*# mm3

-------------------------------------------------------------------------------------------------------------------------------

---------

MEMBER PARAMETERS:

L, = #"!"" mm 8L,/r, = 2"!4$ Lb = #"!"" mm

L = #"!"" mm 8L/r = #! Cb = !""

-------------------------------------------------------------------------------------------------------------------------------

---------INTERNAL FORCES: NOMINAL STRENGTHS:

Mux = -$!"1 .f(mm fu:,Bmx = 2!1#"4 .f/cm2

9u = 1$1!2$23 .f fu:Bmx = 2!2"$ .f/cm2 9n = 3$"#3!*22

.f

Mu, = 3#$1!4$4 .f(mm Vu, = -*3!"*$# .f Mn, =

2$341$!*3$1# .f(mm Vn, = 3"!*32 .f

Mu = -2131!413$" .f(mm Vu = -#2#!#1#2 .f Mn =

$"1#3!#3 .f(mm Vn = 4"!431# .f

-------------------------------------------------------------------------------------------------------------------------------

---------

COEFFICIENTS:

+i b = "!4" +i c = "!#$ +i : = "!4"

----------------------------------------------------------------------------------------------------------------------------------------

SECTION ELEMENTS:

;NS = Com ) Mu/+ib(Mn>> = "!3" ? !"" L@+D A-&>

Vu,/+i:(Vn,> ) fu:,Bmx/"!*(+i:(+,> = "!" ? !"" Vu/+i:(Vn> ) fu:Bmx/"!*(+i:(+,> = "!"$ ?

!"" L@+D +2-2> A2-2>

-------------------------------------------------------------------------------------------------------------------------------

---------

LIMIT DISPLACEMENTS


Displacements

:x = " mm ? :x max = L/$"!"" = # mm Verifie0


:, = " mm ? :, max = L/$"!"" = # mm Verifie0


-------------------------------------------------------------------------------------------------------------------------------

---------

Section OK !!!

STEEL DESIGN-------------------------------------------------------------------------------------------------------------------------------



50/221


#alculo $structural Autodes% &obot Structural" Pg. !0

---------


--------------

calculo estructural final.docx

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