A maior rede de estudos do Brasil

Grátis
168 pág.
Desenvolvimento de Software para DImensionamento Otimizado de Porticos Espaciais em Estruturas de Metalicas

Pré-visualização | Página 37 de 38

limits 
fma(1) fmr(2) faa(3) far(4) 
xy plane Secant - L / 300 - - 
xz plane Secant - L / 300 - - 
Notation: 
(1) Absolute maximum deflection 
(2) Relative maximum deflection 
(3) Absolute active deflection 
(4) Relative active deflection 
 
 
Fixity coefficients 
 Origin End 
xy plane 1.000 1.000 
xz plane 1.000 1.000 
 
 
 
Code checks 
 Resistance use: 46.34 % 
 Deflection use: 7.26 % 
 
 
 
 
 
 
http://www.novapdf.com
 
 
Bar N8 / N3 
Section: CVS 500x194 
Material: Steel (A-572 345MPa) 
 
Nodes Length 
(m) 
Rotation angle 
(degrees) 
Theoretic weight 
(kgf) Initial Final 
N8 N3 3.000 0.000 581.69 
 
 
 
Buckling 
 
Buckling Lateral buckling 
xy plane xz plane Top fl. Bot. fl. 
 (1) 1.00 1.00 1.00 1.00 
LK (2) 3.000 3.000 3.000 3.000 
Cb (3) - 1.000 
Notation: 
(1) Buckling coefficient 
(2) Buckling length (m) 
(3) Critical moment modification factor Cb 
 
 
Deflection group: G8 
 Type 
Deflection limits 
fma(1) fmr(2) faa(3) far(4) 
xy plane Secant - L / 300 - - 
xz plane Secant - L / 300 - - 
Notation: 
(1) Absolute maximum deflection 
(2) Relative maximum deflection 
(3) Absolute active deflection 
(4) Relative active deflection 
 
 
Fixity coefficients 
 Origin End 
xy plane 1.000 1.000 
xz plane 1.000 1.000 
 
 
 
Code checks 
 Resistance use: 46.34 % 
 Deflection use: 7.26 % 
 
 
 
 
http://www.novapdf.com
 
Bar N2 / N9 
Section: CVS 500x194 
Material: Steel (A-572 345MPa) 
 
Nodes Length 
(m) 
Rotation angle 
(degrees) 
Theoretic weight 
(kgf) Initial Final 
N2 N9 3.000 0.000 581.68 
 
 
 
Buckling 
 
Buckling Lateral buckling 
xy plane xz plane Top fl. Bot. fl. 
 (1) 1.00 1.00 1.00 1.00 
LK (2) 3.000 3.000 3.000 3.000 
Cb (3) - 1.000 
Notation: 
(1) Buckling coefficient 
(2) Buckling length (m) 
(3) Critical moment modification factor Cb 
 
 
Deflection group: G9 
 Type 
Deflection limits 
fma(1) fmr(2) faa(3) far(4) 
xy plane Secant - L / 300 - - 
xz plane Secant - L / 300 - - 
Notation: 
(1) Absolute maximum deflection 
(2) Relative maximum deflection 
(3) Absolute active deflection 
(4) Relative active deflection 
 
 
Fixity coefficients 
 Origin End 
xy plane 1.000 1.000 
xz plane 1.000 1.000 
 
 
 
Code checks 
 Resistance use: 74.71 % 
 Deflection use: 11.93 % 
 
 
 
 
http://www.novapdf.com
 
Bar N9 / N10 
Section: CVS 650x234 
Material: Steel (A-572 345MPa) 
 
Nodes Length 
(m) 
Rotation angle 
(degrees) 
Theoretic weight 
(kgf) Initial Final 
N9 N10 10.000 0.000 2342.69 
 
 
 
Buckling 
 
Buckling Lateral buckling 
xy plane xz plane Top fl. Bot. fl. 
 (1) 1.00 1.00 1.00 1.00 
LK (2) 10.000 10.000 10.000 10.000 
Cb (3) - 1.000 
Notation: 
(1) Buckling coefficient 
(2) Buckling length (m) 
(3) Critical moment modification factor Cb 
 
 
Deflection group: G10 
 Type 
Deflection limits 
fma(1) fmr(2) faa(3) far(4) 
xy plane Secant - L / 300 - - 
xz plane Secant - L / 300 - - 
Notation: 
(1) Absolute maximum deflection 
(2) Relative maximum deflection 
(3) Absolute active deflection 
(4) Relative active deflection 
 
 
Fixity coefficients 
 Origin End 
xy plane 1.000 1.000 
xz plane 1.000 1.000 
 
 
 
Code checks 
 Resistance use: 24.46 % 
 Deflection use: 17.82 % 
 
 
 
 
 
 
http://www.novapdf.com
 
 
Bar N10 / N11 
Section: CVS 650x234 
Material: Steel (A-572 345MPa) 
 
Nodes Length 
(m) 
Rotation angle 
(degrees) 
Theoretic weight 
(kgf) Initial Final 
N10 N11 10.000 0.000 2342.69 
 
 
 
Buckling 
 
Buckling Lateral buckling 
xy plane xz plane Top fl. Bot. fl. 
 (1) 1.00 1.00 1.00 1.00 
LK (2) 10.000 10.000 10.000 10.000 
Cb (3) - 1.000 
Notation: 
(1) Buckling coefficient 
(2) Buckling length (m) 
(3) Critical moment modification factor Cb 
 
 
Deflection group: G11 
 Type 
Deflection limits 
fma(1) fmr(2) faa(3) far(4) 
xy plane Secant - L / 300 - - 
xz plane Secant - L / 300 - - 
Notation: 
(1) Absolute maximum deflection 
(2) Relative maximum deflection 
(3) Absolute active deflection 
(4) Relative active deflection 
 
 
Fixity coefficients 
 Origin End 
xy plane 1.000 1.000 
xz plane 1.000 1.000 
 
 
 
Code checks 
 Resistance use: 32.66 % 
 Deflection use: 27.00 % 
 
 
 
 
 
 
http://www.novapdf.com
 
 
Bar N12 / N11 
Section: CVS 650x234 
Material: Steel (A-572 345MPa) 
 
Nodes Length 
(m) 
Rotation angle 
(degrees) 
Theoretic weight 
(kgf) Initial Final 
N12 N11 10.000 0.000 2342.69 
 
 
 
Buckling 
 
Buckling Lateral buckling 
xy plane xz plane Top fl. Bot. fl. 
 (1) 1.00 1.00 1.00 1.00 
LK (2) 10.000 10.000 10.000 10.000 
Cb (3) - 1.000 
Notation: 
(1) Buckling coefficient 
(2) Buckling length (m) 
(3) Critical moment modification factor Cb 
 
 
Deflection group: G12 
 Type 
Deflection limits 
fma(1) fmr(2) faa(3) far(4) 
xy plane Secant - L / 300 - - 
xz plane Secant - L / 300 - - 
Notation: 
(1) Absolute maximum deflection 
(2) Relative maximum deflection 
(3) Absolute active deflection 
(4) Relative active deflection 
 
 
Fixity coefficients 
 Origin End 
xy plane 1.000 1.000 
xz plane 1.000 1.000 
 
 
 
Code checks 
 Resistance use: 24.46 % 
 Deflection use: 17.82 % 
 
 
 
 
http://www.novapdf.com
 
Bar N9 / N12 
Section: CVS 650x234 
Material: Steel (A-572 345MPa) 
 
Nodes Length 
(m) 
Rotation angle 
(degrees) 
Theoretic weight 
(kgf) Initial Final 
N9 N12 10.000 0.000 2342.69 
 
 
 
Buckling 
 
Buckling Lateral buckling 
xy plane xz plane Top fl. Bot. fl. 
 (1) 1.00 1.00 1.00 1.00 
LK (2) 10.000 10.000 10.000 10.000 
Cb (3) - 1.000 
Notation: 
(1) Buckling coefficient 
(2) Buckling length (m) 
(3) Critical moment modification factor Cb 
 
 
Deflection group: G13 
 Type 
Deflection limits 
fma(1) fmr(2) faa(3) far(4) 
xy plane Secant - L / 300 - - 
xz plane Secant - L / 300 - - 
Notation: 
(1) Absolute maximum deflection 
(2) Relative maximum deflection 
(3) Absolute active deflection 
(4) Relative active deflection 
 
 
Fixity coefficients 
 Origin End 
xy plane 1.000 1.000 
xz plane 1.000 1.000 
 
 
 
Code checks 
 Resistance use: 32.66 % 
 Deflection use: 27.00 % 
 
 
 
 
http://www.novapdf.com
 
Bar N5 / N12 
Section: CVS 500x194 
Material: Steel (A-572 345MPa) 
 
Nodes Length 
(m) 
Rotation angle 
(degrees) 
Theoretic weight 
(kgf) Initial Final 
N5 N12 3.000 0.000 581.68 
 
 
 
Buckling 
 
Buckling Lateral buckling 
xy plane xz plane Top fl. Bot. fl. 
 (1) 1.00 1.00 1.00 1.00 
LK (2) 3.000 3.000 3.000 3.000 
Cb (3) - 1.000 
Notation: 
(1) Buckling coefficient 
(2) Buckling length (m) 
(3) Critical moment modification factor Cb 
 
 
Deflection group: G14 
 Type 
Deflection limits 
fma(1) fmr(2) faa(3) far(4) 
xy plane Secant - L / 300 - - 
xz plane Secant - L / 300 - - 
Notation: 
(1) Absolute maximum deflection 
(2) Relative maximum deflection 
(3) Absolute active deflection 
(4) Relative active deflection 
 
 
Fixity coefficients 
 Origin End 
xy plane 1.000 1.000 
xz plane 1.000 1.000 
 
 
 
Code checks 
 Resistance use: 74.71 % 
 Deflection use: 11.93 % 
 
 
 
 
http://www.novapdf.com
 
Bar N4 / N11 
Section: CVS 500x194 
Material: Steel (A-572 345MPa) 
 
Nodes Length 
(m) 
Rotation angle 
(degrees) 
Theoretic weight 
(kgf) Initial Final 
N4 N11 3.000 0.000 581.68 
 
 
 
Buckling 
 
Buckling Lateral buckling 
xy plane xz plane Top fl. Bot. fl. 
 (1) 1.00 1.00 1.00 1.00 
LK (2) 3.000 3.000 3.000 3.000 
Cb (3) - 1.000 
Notation: 
(1) Buckling coefficient 
(2) Buckling length (m) 
(3) Critical moment modification factor Cb 
 
 
Deflection group: G15 
 Type 
Deflection limits 
fma(1) fmr(2) faa(3) far(4) 
xy plane Secant - L / 300 - - 
xz plane Secant - L / 300 - - 
Notation: 
(1) Absolute maximum deflection 
(2) Relative maximum deflection 
(3) Absolute active deflection 
(4) Relative active deflection 
 
 
Fixity coefficients 
 Origin End 
xy plane 1.000 1.000 
xz plane 1.000 1.000 
 
 
 
Code checks 
 Resistance use: 74.71 % 
 Deflection