# pdf-155894258-pressure-vessel-design-excel-sheet-basic-designing-non-critical-p-xls compress

```Basic Data Input
Inner Diameter of Shell
Length of Shell
!hic&quot;ness of Shell
!hic&quot;ness of !o\$ % Left &amp;nd 1
!hic&quot;ness of 'ottom % Right &amp;nd 2
(ean Diameter of Shell
!+\$e of !o\$ % Left &amp;nd 1
!+\$e of 'ottom % Right &amp;nd 2
S\$ecific rait+ of material
4ressure
4ressure
Stress alue
7oint &amp;fficienc+
)orrosion allo*ance
1,100
550
3,120
12.0
12.0
12.0
1,112
&amp;
&amp;
/.5
5
5.
20,000
0.5
0.0
Determine Thic#ness of \$essel
Re9uired thic&quot;ness of Shell
2./:
Re9uired thic&quot;ness of &amp;nd -&amp;
2./5
Re9uired thic&quot;ness of &amp;nd -! :;
0.00
Re9uired thic&quot;ness of &amp;nd -! 10;
0.00
Re9uired thic&quot;ness of &amp;nd -6
0.00
Re9uired th&quot; of &amp;nd -) Longit&lt;l
0.00
Re9uired th&quot; of &amp;nd -) )ircumf&lt;l
0.00
)o&gt;efficient ( re9d. for &amp;nd -! 10;
0.00
Properties of Top / Left End 1
mm
mm
mm
mm
mm
mm
mm
\$si
&quot;g%cm
\$si
mm
mm
mm
mm
mm
mm
mm
mm
&amp;a'imum Pressure alloa)le in \$essel
4ressure
3::
\$si
6+drotest 4ressure
=/:
\$si
4ressure
25./=
&quot;g%cm
6+drotest 4ressure
33.=:
&quot;g%cm
4ressure
2.52
(4a
6+drotest 4ressure
3.2
(4
(4a
+,TE% #g/cm-. )ar.
)ar. atmosphere are almost same
\$olume hen \$essel i0e is gien
Volume of Shell
2.:5
Volume of !o\$ % Left &amp;nd 1
0.222
Volume of 'ottom % Right &amp;nd 2
0.222
Volume of essel
3.=0
m&sup3;
m&sup3;
m&sup3;
m&sup3;
eight of \$essel
?rea of Shell
11.02
?rea of !o\$ % Left )one &amp;nd 1
1.=:
?rea of 'ottom % Right
Right )one &amp;nd 2
1.=:
m
m
m
!otal Surface ?rea of Vessel
#eight of Shell
#eight of !o\$ % Left end 1
#eight of 'ottom % Right end 2
!otal #eight
m
&quot;gs
&quot;gs
&quot;gs
&quot;gs
13.=
1,02:./
13/.=5
13/.=5
1,301.//
Properties of Bottom / Right End 2
Hemispherical (H
Volume
0.000
Surface area
0.000
#eight of end
0.00
m&sup3;
m
&quot;gs
Volume
Surface area
#eight of end
! &quot; D / Torispherical (T
0
0
1/0
S -default
0
S -actual
50
6t. of end -incl. S
0
Volume
0.000
Surface area
0.000
'lan&quot; si8e
0
#eight of end
0.00
mm
mm
mm
mm
mm
mm
m&sup3;
m
dia
&quot;gs
! &quot; D / Torispherical (T
0
0
1/0
S -default
0
S -actual
50
6t. of end -incl. S
0
Volume
0.000
Surface area
0.000
'lan&quot; si8e
0
#eight of end
0.00
mm
mm
mm
mm
mm
mm
m&sup3;
m
dia
&quot;gs
2%1 Ellipsoidal (E
0
1/
6t. of end
2/5
S
50
6t. of end -incl. S
325
Volume of S
0.0=
Volume !otal
0.222
Surface area
1.=5
mm
mm
mm
mm
mm
m&sup3;
m&sup3;
m
2%1 Ellipsoidal (E
0
1/
6t. of end
2/5
S
50
6t. of end -incl. S
325
Volume of S
0.0=
Volume !otal
0.222
Surface area
1.=5
mm
mm
mm
mm
mm
m&sup3;
m&sup3;
m
'lan&quot; si8e
#eight of end
13:3
13/.=5
dia
&quot;gs
'lan&quot; si8e
#eight of end
13:3
13/.=5
dia
&quot;gs
Truncated *one (T*
Small diameter
200
00
6t. of cone
Volume
0.000
'ig diameter -outer
0
Small diameter -outer
0
Surface area
0.000
#eight of end
0.00
mm
mm
m&sup3;
mm
mm
m
&quot;gs
Truncated *one (T*
Small diameter
150
6t. of cone
00
Volume
0.000
'ig diameter -outer
0
Small diameter -outer
0
Surface area
0.000
#eight of end
0.00
mm
mm
m&sup3;
mm
mm
m
&quot;gs
!ull *one (*
6t. of cone
00
Volume
0.000
'ig diameter -outer
0
?\$e@ angle -d
-degrees
egrees
0.000
?\$e@ angle -ra
dians
0.000
Surface area
0.000
#eight of end
m
!ull *one
6t. of cone
Volume
'ig diameter -outer
?\$e@ angle -degrees
Surface area
0.00
&quot;gs
#eight of end
0.000
0.000
0.00
m&sup3;
m
&quot;gs
Volume
Surface area
#eight of end
mm
m&sup3;
mm
!lat (!
Volume
Surface area
#eight of end
Hemispherical (H
0.000
0.000
0.00
(*
00
0.000
0
0.000
0.000
0.000
m&sup3;
m
&quot;gs
mm
m&sup3;
mm
m
0.00
&quot;gs
0.000
0.000
0.00
m&sup3;
m
&quot;gs
!lat (!
```