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Rectangular Tank Calculation Sheet
TANK CALCULATION SHEET I. DESIGN PARAMETERS: - Code Design
: API 650 & Roark's Formulas Pd : Full water
- Design pressure - Design temperature - Operating pressure - Operating temperature - Corrosion Allowance - Liquid Specific Gravity - Joint Efficiency - Elastic Modulus
MATERIAL SPECIFICATION - Shell, Roof & Bottom - Allowable Stress
= 14.72 kPa : 60 oC / AMB : ATM o : AMB C C.A : 1.5 mm : 0.88 : 0.85 (For Shell) : 0.85 (For Roof & Bottom) E : 2.91*E+7 psi = 200637437 kPa RECTANGULAR : : A-36 Sa : 16600 psi = 114453 kPa : A-106 Gr. B : A-105 : A-234 Gr. WPB : A-193 Gr. B7 / A-194 Gr. 2H : A-36
- Nozzle Neck - Flange - Pipe Fittings - Bolts & Nuts - Stiffeners TANK GEOMETRY: - Height - Length - Width
Height (H)
H: L: W:
Width (W)
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1500 mm 1500 mm 1500 mm
Rectangular Tank Calculation Sheet
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Rectangular Tank Calculation Sheet II. DESIGN II.1 Side Wall Plate Calculation (Height x Length) II.1.1 Wall Thickness Calculation (As per Roark's Formulas 7th Ed, Table 11.4 Case 1a)
b
b
b
a
a
a
Height (H)
a
b
Stiffeners
Length (L)
Vertical length without reinforced Horizontal length without reinforced Ratio, α β Required thickness tr = Sqrt(β*Pd*b2)/Sa) + C.A
a: b: a/b : = =
750 mm 750 mm 1.00 0.0444 0.2874
= ta :
6.06 mm 8.00 mm
=
2.01 mm
II.1.2 Top Edge Stiffener R1 = 0.03*Pd*a
=
0.33 kN/m
R2 = 0.32*Pd*a
=
3.53 kN/m
Adopted thickness Maximum deflection Ymax = α*Pd*b4/(E*ta3) Ymax
1/2 ta < 2.01mm < 4mm Therefore, adopted thickness is satisfactory
Moment inertia required: Jmin = R1*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x8): Jx = Jy =
339.93 mm4 0.0340 cm4 38.285 cm4
Therefore, Top edge stiffener is satisfactory II.1.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x8): Jx = Jy = Therefore, Horizontal stiffener is satisfactory
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3625.88 mm4 0.3626 cm4 38.285 cm4
Rectangular Tank Calculation Sheet
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Rectangular Tank Calculation Sheet II.1.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2
=
432.98 mm
=
0.13 kNm
= = Section modulus of used stiffener (angle 65x65x8): Z = Therefore, Vertical stiffener is satisfactory
1.16E-06 mm3 1.16 cm3
Required section modulus: Zr = Mmax/Sa
7.96 cm3
II.2 Side Wall Plate Calculation (Height x Width) II.2.1 Wall Thickness Calculation (As per Roark's Formulas 7th Ed, Table 11.4 Case 1a) b
b
b
a
a
a
Height (H)
a
b
Stiffeners
Width (W) Vertical length without reinforced Horizontal length without reinforced Ratio, α β Required thickness tr = Sqrt(β*Pd*b2)/Sa) + C.A
a: b: a/b : = =
750 mm 750 mm 1.00 0.0444 0.2874
= ta :
6.06 mm 8.00 mm
=
2.01 mm
II.2.2 Top Edge Stiffener R1 = 0.03*Pd*a
=
0.33 kN/m
R2 = 0.32*Pd*a
=
3.53 kN/m
Adopted thickness Maximum deflection Ymax = α*Pd*b4/(E*ta3) Ymax
1/2 ta < 2.01mm < 4mm Therefore, adopted thickness is satisfactory
Moment inertia required: Jmin = R1*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x8): Jx = Jy = Therefore, Top edge stiffener is satisfactory Page 5 of 27
339.93 mm4 0.0340 cm4 38.285 cm4
Rectangular Tank Calculation Sheet
II.2.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x8): Jx = Jy =
3625.88 mm4 0.3626 cm4 38.285 cm4
Therefore, Horizontal stiffener is satisfactory II.2.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2
=
432.98 mm
=
0.13 kNm
= = Section modulus of used stiffener (angle 65x65x8): Z = Therefore, Vertical stiffener is satisfactory
1.16E-06 mm3 1.16 cm3
Required section modulus: Zr = Mmax/Sa
7.96 cm3
II.3 Roof Plate Calculation b
a
Width (W)
a
b
Stiffeners
Length (L)
Loads on roof plate: - Roof area: - Live load: - Roof weight: - Roof structure weight: - Roof Equipment weight: - Dead load: Total load on roof plate: Distance without reinforced in width Distance without reinforced in length Ratio, α β Required thickness: tr = Sqrt(β*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection:
= = = = = = =
2.25 m2 1.5 kPa 156 kg 116 kg 100 kg 1.6 kPa 3.1 kPa
a: b: a/b : = =
1500 mm 1500 mm 1.00 0.0444 0.2874
= ta :
5.70 mm 10.00 mm
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Rectangular Tank Calculation Sheet Ymax = α*Pd*b4/(E*ta3)
=
Ymax
1/2 ta < 3.5mm < 5mm Therefore, adopted thickness is satisfactory
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3.50 mm
Rectangular Tank Calculation Sheet b
b
b
a
a
a
Width (W)
a
II.4 Bottom Plate Calculation b
Stiffeners
Length (L) Distance without reinforced in width Distance without reinforced in length Ratio, α β Required thickness: tr = Sqrt(β*Pd*b2)/Sa) + C.A
a: b: a/b : = =
750.0 mm 750.0 mm 1.00 0.0444 0.2874
= ta :
6.06 mm 8.00 mm
=
2.01 mm
Adopted thickness Maximum deflection: Ymax = α*Pd*b4/(E*ta3) Ymax
1/2 ta
< 2.01mm < 4mm Therefore, adopted thickness is satisfactory
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Rectangular Tank Calculation Sheet
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Rectangular Tank Calculation Sheet
TANK CALCULATION SHEET I. DESIGN PARAMETERS: - Code Design
: API 650 & Roark's Formulas Pd : Full water
- Design pressure - Design temperature - Operating pressure - Operating temperature - Corrosion Allowance - Liquid Specific Gravity - Joint Efficiency - Elastic Modulus
MATERIAL SPECIFICATION - Shell, Roof & Bottom - Allowable Stress
= 19.62 kPa : 60 oC / AMB : ATM o : AMB C C.A : 1.5 mm : 0.88 : 0.85 (For Shell) : 0.85 (For Roof & Bottom) E : 2.91*E+7 psi = 200637437 kPa RECTANGULAR : : A-36 Sa : 16600 psi = 114453 kPa : A-106 Gr. B : A-105 : A-234 Gr. WPB : A-193 Gr. B7 / A-194 Gr. 2H : A-36
- Nozzle Neck - Flange - Pipe Fittings - Bolts & Nuts - Stiffeners TANK GEOMETRY: - Height - Length - Width
Height (H)
H: L: W:
Width (W)
Page 10 of 27
2000 mm 1000 mm 1000 mm
Rectangular Tank Calculation Sheet
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Rectangular Tank Calculation Sheet II. DESIGN II.1 Side Wall Plate Calculation (Height x Length) II.1.1 Wall Thickness Calculation (As per Roark's Formulas 7th Ed, Table 11.4 Case 1a)
b
b
b
a
a
a
Height (H)
a
b
Stiffeners
Length (L)
Vertical length without reinforced Horizontal length without reinforced Ratio, α β Required thickness tr = Sqrt(β*Pd*b2)/Sa) + C.A
a: b: a/b : = =
1000 mm 500 mm 2.00 0.111 0.6102
= ta :
6.61 mm 8.00 mm
=
1.33 mm
II.1.2 Top Edge Stiffener R1 = 0.03*Pd*a
=
0.59 kN/m
R2 = 0.32*Pd*a
=
6.28 kN/m
Adopted thickness Maximum deflection Ymax = α*Pd*b4/(E*ta3) Ymax
1/2 ta < 1.33mm < 4mm Therefore, adopted thickness is satisfactory
Moment inertia required: Jmin = R1*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x6): Jx = Jy =
119.37 mm4 0.0119 cm4 38.285 cm4
Therefore, Top edge stiffener is satisfactory II.1.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x6): Jx = Jy =
1273.29 mm4 0.1273 cm4
Therefore, Horizontal stiffener is satisfactory
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38.285 cm4
Rectangular Tank Calculation Sheet
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Rectangular Tank Calculation Sheet II.1.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2
=
577.30 mm
=
0.21 kNm
= = Section modulus of used stiffener (angle 65x65x6): Z = Therefore, Vertical stiffener is satisfactory
1.83E-06 mm3 1.83 cm3
Required section modulus: Zr = Mmax/Sa
7.96 cm3
II.2 Side Wall Plate Calculation (Height x Width) II.2.1 Wall Thickness Calculation (As per Roark's Formulas 7th Ed, Table 11.4 Case 1a) b
b
b
a
a
a
Height (H)
a
b
Stiffeners
Width (W) Vertical length without reinforced Horizontal length without reinforced Ratio, α β Required thickness tr = Sqrt(β*Pd*b2)/Sa) + C.A
a: b: a/b : = =
1000 mm 500 mm 2.00 0.111 0.6102
= ta :
6.61 mm 8.00 mm
=
1.33 mm
II.2.2 Top Edge Stiffener R1 = 0.03*Pd*a
=
0.59 kN/m
R2 = 0.32*Pd*a
=
6.28 kN/m
Adopted thickness Maximum deflection Ymax = α*Pd*b4/(E*ta3) Ymax
1/2 ta < 1.33mm < 4mm Therefore, adopted thickness is satisfactory
Moment inertia required: Jmin = R1*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x6): Jx = Jy = Therefore, Top edge stiffener is satisfactory Page 14 of 27
119.37 mm4 0.0119 cm4 38.285 cm4
Rectangular Tank Calculation Sheet
II.2.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x6): Jx = Jy =
1273.29 mm4 0.1273 cm4 38.285 cm4
Therefore, Horizontal stiffener is satisfactory II.2.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2
=
577.30 mm
=
0.21 kNm
= = Section modulus of used stiffener (angle 65x65x8): Z = Therefore, Vertical stiffener is satisfactory
1.83E-06 mm3 1.83 cm3
Required section modulus: Zr = Mmax/Sa
7.96 cm3
II.3 Roof Plate Calculation b
a
Width (W)
a
b
Stiffeners
Length (L)
Loads on roof plate: - Roof area: - Live load: - Roof weight: - Roof structure weight: - Roof Equipment weight: - Dead load: Total load on roof plate: Distance without reinforced in width Distance without reinforced in length Ratio, α β Required thickness: tr = Sqrt(β*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection:
= = = = = = =
1 m2 1.5 kPa 97 kg 116 kg 100 kg 3.1 kPa 4.6 kPa
a: b: a/b : = =
1000 mm 1000 mm 1.00 0.0444 0.2874
= ta :
4.89 mm 8.00 mm
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Rectangular Tank Calculation Sheet Ymax = α*Pd*b4/(E*ta3)
=
Ymax
1/2 ta < 1.97mm < 4mm Therefore, adopted thickness is satisfactory
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1.97 mm
Rectangular Tank Calculation Sheet b
b
b
a
a
a
Width (W)
a
II.4 Bottom Plate Calculation b
Stiffeners
Length (L) Distance without reinforced in width Distance without reinforced in length Ratio, α β Required thickness: tr = Sqrt(β*Pd*b2)/Sa) + C.A
a: b: a/b : = =
500.0 mm 500.0 mm 1.00 0.444 0.2874
= ta :
5.01 mm 10.00 mm
=
2.71 mm
Adopted thickness Maximum deflection: Ymax = α*Pd*b4/(E*ta3) Ymax
1/2 ta
< 2.71mm < 5mm Therefore, adopted thickness is satisfactory
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Rectangular Tank Calculation Sheet
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Rectangular Tank Calculation Sheet
TANK CALCULATION SHEET I. DESIGN PARAMETERS: - Code Design
: API 650 & Roark's Formulas Pd : Full water + 25 Psig
- Design pressure - Design temperature - Operating pressure - Operating temperature - Corrosion Allowance - Liquid Specific Gravity - Joint Efficiency - Elastic Modulus
MATERIAL SPECIFICATION - Shell, Roof & Bottom - Allowable Stress
= 36.86 kPa : 65.6 oC / AMB : ATM o : AMB C C.A : 1.5 mm : 0.88 : 0.85 (For Shell) : 0.85 (For Roof & Bottom) E : 2.91*E+7 psi = 200637437 kPa RECTANGULAR : : A-36 Sa : 16600 psi = 114453 kPa : A-106 Gr. B : A-105 : A-234 Gr. WPB : A-193 Gr. B7 / A-194 Gr. 2H : A-36
- Nozzle Neck - Flange - Pipe Fittings - Bolts & Nuts - Stiffeners TANK GEOMETRY: - Height - Length - Width
Height (H)
H: L: W:
Width (W)
Page 19 of 27
2000 mm 2000 mm 2000 mm
Rectangular Tank Calculation Sheet
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Rectangular Tank Calculation Sheet II. DESIGN II.1 Side Wall Plate Calculation (Height x Length) II.1.1 Wall Thickness Calculation (As per Roark's Formulas 7th Ed, Table 11.4 Case 1a)
b
b
b
a
a
a
Height (H)
a
b
Stiffeners
Length (L)
Vertical length without reinforced Horizontal length without reinforced Ratio, α β Required thickness tr = Sqrt(β*Pd*b2)/Sa) + C.A
a: b: a/b : = =
500 mm 500 mm 1.00 0.0444 0.2874
= ta :
6.31 mm 8.00 mm
=
1.00 mm
II.1.2 Top Edge Stiffener R1 = 0.03*Pd*a
=
0.55 kN/m
R2 = 0.32*Pd*a
=
5.90 kN/m
Adopted thickness Maximum deflection Ymax = α*Pd*b4/(E*ta3) Ymax
1/2 ta < 1mm < 4mm Therefore, adopted thickness is satisfactory
Moment inertia required: Jmin = R1*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x8): Jx = Jy =
112.12 mm4 0.0112 cm4 38.285 cm4
Therefore, Top edge stiffener is satisfactory II.1.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x8): Jx = Jy =
1195.93 mm4 0.1196 cm4
Therefore, Horizontal stiffener is satisfactory
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38.285 cm4
Rectangular Tank Calculation Sheet
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Rectangular Tank Calculation Sheet II.1.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2
=
288.65 mm
=
0.10 kNm
= = Section modulus of used stiffener (angle 65x65x8): Z = Therefore, Vertical stiffener is satisfactory
8.60E-07 mm3 0.86 cm3
Required section modulus: Zr = Mmax/Sa
7.96 cm3
II.2 Side Wall Plate Calculation (Height x Width) II.2.1 Wall Thickness Calculation (As per Roark's Formulas 7th Ed, Table 11.4 Case 1a) b
b
b
a
a
a
Height (H)
a
b
Stiffeners
Width (W) Vertical length without reinforced Horizontal length without reinforced Ratio, α β Required thickness tr = Sqrt(β*Pd*b2)/Sa) + C.A
a: b: a/b : = =
400 mm 400 mm 1.00 0.444 0.2874
= ta :
5.35 mm 10.00 mm
=
2.09 mm
II.2.2 Top Edge Stiffener R1 = 0.03*Pd*a
=
0.44 kN/m
R2 = 0.32*Pd*a
=
4.72 kN/m
Adopted thickness Maximum deflection Ymax = α*Pd*b4/(E*ta3) Ymax
1/2 ta < 2.09mm < 5mm Therefore, adopted thickness is satisfactory
Moment inertia required: Jmin = R1*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x8): Jx = Jy = Therefore, Top edge stiffener is satisfactory Page 23 of 27
29.39 mm4 0.0029 cm4 38.285 cm4
Rectangular Tank Calculation Sheet
II.2.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= = Moment inertia of used stiffener (angle 65x65x8): Jx = Jy =
313.51 mm4 0.0314 cm4 38.285 cm4
Therefore, Horizontal stiffener is satisfactory II.2.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2
=
230.92 mm
=
0.05 kNm
= = Section modulus of used stiffener (angle 65x65x8): Z = Therefore, Vertical stiffener is satisfactory
4.40E-07 mm3 0.44 cm3
Required section modulus: Zr = Mmax/Sa
7.96 cm3
II.3 Roof Plate Calculation b
a
Width (W)
a
b
Stiffeners
Length (L)
Loads on roof plate: - Roof area: - Live load: - Roof weight: - Roof structure weight: - Roof Equipment weight: - Dead load: Total load on roof plate: Distance without reinforced in width Distance without reinforced in length Ratio, α β Required thickness: tr = Sqrt(β*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection:
= = = = = = =
4 m2 1.5 kPa 238 kg 116 kg 100 kg 1.1 kPa 2.6 kPa
a: b: a/b : = =
1000 mm 1000 mm 1.00 0.444 0.2874
= ta :
4.06 mm 12.00 mm
Page 24 of 27
Rectangular Tank Calculation Sheet Ymax = α*Pd*b4/(E*ta3)
=
Ymax
1/2 ta < 3.35mm < 6mm Therefore, adopted thickness is satisfactory
Page 25 of 27
3.35 mm
Rectangular Tank Calculation Sheet II.4 Bottom Plate Calculation b
b
b
a
a
a
Width (W)
a
b
Stiffeners
Length (L) Distance without reinforced in width Distance without reinforced in length Ratio, α β Required thickness: tr = Sqrt(β*Pd*b2)/Sa) + C.A
a: b: a/b : = =
400.0 mm 400.0 mm 1.00 0.444 0.2874
= ta :
5.35 mm 10.00 mm
=
2.09 mm
Adopted thickness Maximum deflection: Ymax = α*Pd*b4/(E*ta3) Ymax
1/2 ta
< 2.09mm < 5mm Therefore, adopted thickness is satisfactory
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Rectangular Tank Calculation Sheet
Page 27 of 27