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análise de tensões atuantes em junções bocais/casco de vasos de ...

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(Stresses parallel to Top Top Bottom Bottom<br />

longitudinal plane) Outsi<strong>de</strong> Insi<strong>de</strong> Outsi<strong>de</strong> Insi<strong>de</strong><br />

-----------( )------------<br />

Inplane M<strong>em</strong>brane (P ) 1 1 1 1<br />

Inplane Bending (P ) 10 -10 10 -10<br />

Inplane M<strong>em</strong>brane (Mc) 0 0 0 0<br />

Inplane Bending (Mc) 0 0 0 0<br />

Inplane M<strong>em</strong>brane (ML) -2 -2 2 2<br />

Inplane Bending (ML) -11 11 11 -11<br />

Inplane Pressure Stress 50 50 50 50<br />

----------------------- -------- -------- -------- --------<br />

Inplane Stress Summary 48 50 76 31<br />

VESSEL Stresses<br />

LONGITUDINAL PLANE Au Al Bu Bl<br />

(Shear stress normal to Top Top Bottom Bottom<br />

longitudinal plane) Outsi<strong>de</strong> Insi<strong>de</strong> Outsi<strong>de</strong> Insi<strong>de</strong><br />

-----------( )------------<br />

Outplane Shear (Vc) 0 0 0 0<br />

Outplane Shear (Vl) 0 0 0 0<br />

Outplane Shear (Mt) 0 0 0 0<br />

----------------------- -------- -------- -------- --------<br />

Shear Stress Summary 0 0 0 0<br />

VESSEL Stresses<br />

LONGITUDINAL PLANE Au Al Bu Bl<br />

(Stress Intensities Top Top Bottom Bottom<br />

Outsi<strong>de</strong> Insi<strong>de</strong> Outsi<strong>de</strong> Insi<strong>de</strong><br />

-----------( )------------<br />

Two * Max Shear Stress 100 102 109 98<br />

VESSEL Stresses<br />

CIRCUMFERENTIAL PLANE Cu Cl Du Dl<br />

(Stresses Normal to Left Left Right Right<br />

circumferential plane) Outsi<strong>de</strong> Insi<strong>de</strong> Outsi<strong>de</strong> Insi<strong>de</strong><br />

-----------( )------------<br />

Outplane M<strong>em</strong>brane (P ) 0 0 0 0<br />

Outplane Bending (P ) 3 -3 3 -3<br />

Outplane M<strong>em</strong>brane (Mc) -1 -1 1 1<br />

Outplane Bending (Mc) -11 11 11 -11<br />

Outplane M<strong>em</strong>brane (ML) 0 0 0 0<br />

Outplane Bending (ML) 0 0 0 0<br />

Normal Pressure Stress 50 50 50 50<br />

----------------------- -------- -------- -------- --------<br />

Outplane Stress Summary 41 58 67 38<br />

VESSEL Stresses<br />

CIRCUMFERENTIAL PLANE Cu Cl Du Dl<br />

(Stresses parallel to Left Left Right Right<br />

circumferential plane) Outsi<strong>de</strong> Insi<strong>de</strong> Outsi<strong>de</strong> Insi<strong>de</strong><br />

-----------( )------------<br />

Inplane M<strong>em</strong>brane (P ) 1 1 1 1<br />

Inplane Bending (P ) 10 -10 10 -10<br />

Inplane M<strong>em</strong>brane (Mc) -2 -2 2 2<br />

Inplane Bending (Mc) -37 37 37 -37<br />

Inplane M<strong>em</strong>brane (ML) 0 0 0 0<br />

Inplane Bending (ML) 0 0 0 0<br />

156

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