análise de tensões atuantes em junções bocais/casco de vasos de ...
análise de tensões atuantes em junções bocais/casco de vasos de ...
análise de tensões atuantes em junções bocais/casco de vasos de ...
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NOZZLE Stresses<br />
CIRCUMFERENTIAL PLANE Cu Cl Du Dl<br />
(Shear stress) Outsi<strong>de</strong> Insi<strong>de</strong> Outsi<strong>de</strong> Insi<strong>de</strong><br />
-----------( )------------<br />
Shear due to (Vc) 0 0 0 0<br />
Shear due to (Vl) -1 -1 1 1<br />
Shear due to Torsion 3 3 3 3<br />
----------------------- -------- -------- -------- --------<br />
Shear Stress Summary 2 2 4 4<br />
NOZZLE Stresses<br />
CIRCUMFERENTIAL PLANE Cu Cl Du Dl<br />
(Stress Intensities Outsi<strong>de</strong> Insi<strong>de</strong> Outsi<strong>de</strong> Insi<strong>de</strong><br />
-----------( )------------<br />
Two * Max Shear Stress 86 67 114 96<br />
Stress Computations at the Edge of the Reinforcing Pad<br />
------------------------------------------------------<br />
WRC 297 Curve Access Parameters:<br />
Tv / Tn = 0.095<br />
Dn / Tn = 10.000<br />
Lambda = [(Dn/Dv)* (Dv/Tv) 1/2 ] = 2.764<br />
Nr/P = 0.068<br />
Mr/P = 0.115<br />
M0/P = 0.034<br />
N0/P = 0.043<br />
MrD/Mc = 0.274<br />
NrDL/Mc = 0.113<br />
M0d/Mc = 0.082<br />
N0DL/Mc = 0.062<br />
MrD/Ml = 0.085<br />
NrDL/Ml = 0.091<br />
M0D/Ml = 0.025<br />
N0DL/Ml = 0.056<br />
VESSEL Stresses<br />
LONGITUDINAL PLANE Au Al Bu Bl<br />
(Stresses 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 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) 0 0 0 0<br />
Outplane Bending (Mc) 0 0 0 0<br />
Outplane M<strong>em</strong>brane (ML) -1 -1 1 1<br />
Outplane Bending (ML) -3 3 3 -3<br />
Normal Pressure Stress 101 102 101 102<br />
----------------------- -------- -------- -------- --------<br />
Outplane Stress Summary 100 102 109 98<br />
VESSEL Stresses<br />
LONGITUDINAL PLANE Au Al Bu Bl<br />
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