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ANALYSIS OF SHELL
STRUCTURES
BY
Anik Kumar Mal
Meghnad Saha Institute of Technology
Department of Civil Engineering
Under the guidance of
Prof. Dr Bimalendu Ghosh
SHELLS
Shell Structure in Civil Engineering
Construction
•The shell structure are very unique
due to its interesting strength to
weight ratio
•They can span over large areas,
while having an exceptionally small
thickness
•Lowers the construction cost
•Aesthetic value
• Curved structure whose
thickness is very less
compared to its span.
• Depth/Radium < 1/20
Classification Of shell
Structures
Analysis of Thin Shell
There are mainly 3 Theories-
• Bending Theory
• Membrane Theory
• Approximation Theory
Analysis of Thin Shell
Bending Theory
• This is the most general & accurate theory.
• This theory is almost applicable in cases
Forces & Moments in Bending Theory:
• 6 Unknown Forces:
• 4 Unknown Moments:
ApproximationTheory,
The Beam Theory
Advantages-
Assumptions:
•The deformation of the cross-section in its plane are
negligible.
•Mx and hence Qx and Mxθ may be ignored.
•The strain γxy caused by the shear force Nxθ and the lateral
contraction are neglected
Analysis By BeamTheory
Nx=longitudinal force
Nxθ=longitudinally varying shear force
Myy=moment about Y axis
Iyy= Moment of intertia about Y-axis
Q= First static moment about Y
Z= depth of neutral axis
d=thickness of shell
V= shear force
Part I
AnalysisBy BeamTheory
Part II
In the 2nd part of analysis the long section of the cylindrical shell have been segmented to
number of elementary arches. The main objective of this analysis is to determine Mθ, Nθ
Computer Program for Beam
Analysis of Cylindrical shell
•The program is made in most general way to solve the shell which is
applicable for shell of any span and of any radius with any semi-
circular angle.
•The program is valid for uniformly distributed dead and live load.
•The program is applicable for any length of span
An analysis of interior shell in a multiple group of shell is done by Beam Theory in book G.
Ramaswami.
The same problem have been analysed with the program for "interior cylindrical shell analysis
in a group of multiple shell"
PROBLEM-
Geometry
span l =62ft
Radius a =31ft
Thickness d =0.3125ft
semicircular angle ф =40°
The shell has no edge beam and uniformly loaded.
Dead load =47lb/
live load =25lb/( Horizontal projection)
Comparison of Result
Comparison of Nx
degree Angle 0 5 10 15 20 25 30 35 40
lb/ft
NX(program) 34099 22392 12058 3178 -4181 -9964 -14127 -16637 -17476
Nx(book) 34145 22421 12074 3183 -4185 -9977 -14144 -16657 -17497
Comparison of Nxθ
degree Angle 0 5 10 15 20 25 30 35 40
lb-ft/ft
Nxθ(program) 0 4910 7896 9204 9094 7836 5710 3001 0
Nxθ(book) 0 4911 7906 9216 9185 7847 5718 3007 0
Comparison of Mθ
degree Angle 0 5 10 15 20 25 30 35 40
lb/ft Mθ(program) -1378 -179.74 477.73 667.03 515.52 172.90 -215.64 -530.7 -694.3
Mθ(book) -1381 -182 475 665 514 173 -215 -526 -687
Comparison of Nθ
degree Angle 0 5 10 15 20 25 30 35 40
lb/ft
Nθ(progra
m)
704.5
7 419.43 -155.50 -873.06 -1606.3 -2251.4 -2728.6 -2983.7 -2989
Nθ(book) 706 420 -156 -875 -1709 -2255 -2733 -2988 -2993
There results obtained from programs are very accurate with less than 1%
variation with book
Comparison between
Beam Theory & Bending
Theory
A problem of simply supported cylindrical shell analysis is
done based on bending theory by following Schorer's approach
in book of J. E. Gibson & B. G. Neil
PROBLEM
Span = 120ft
Radius =30ft
Semicircular angle =40°
load =50lb/ (horizontal projection)
Comparison of Nx
degree Angle(θ) 0 10 20 30 40
lb/ft
NX(beam theory) 86788 30690 -10642 -35955 -44479
Nx(bending theory) 101474 20276 -16684 -29275.8 -31738.3
Comparison of Nxθ
degree Angle(θ) 0 10 20 30 40
lb/ft
Nxθ(beam theory) 0 10048 11572 7266 0
Nxθ(bending theory) 0 7715.6 7577.6 4256.3 0
Comparison of Mθ
degree Angle(θ) 0 10 20 30 40
lb-ft/ft
Mθ(beam theory) 0 429.5 1579.6 2826.8 3561.19
Mθ(bending theory) 0 515.2 1718.6 2855.2 3308.7
Comparison of Nθ
degree Angle(θ) 0 10 20 30 40
lb/ft
Nθ(beam theory) 64 -713.4 -1677.52 -2308.47 -2332.94
Nθ(bending theory) 0 -505.4 -1500.4 -2262.4 -2534.4
Comparison of Q
degree Angle(θ) 0 10 20 30 40
lb/ft
Q(beam theory) 0 0 0 0 0
Q(bending theory) 0 2.4 3.6 2.7 0
-60000
-40000
-20000
0
20000
40000
60000
80000
100000
120000
0 10 20 30 40 50
Nx(lb/ft)
Angle(degree)
Nx variation with θ
0
2000
4000
6000
8000
10000
12000
14000
0 10 20 30 40 50
Nxθ(lb/ft)
Angle (degree)
Nxθ variation with θ
0
500
1000
1500
2000
2500
3000
3500
4000
0 10 20 30 40 50
Mθ(lb-ft/ft)
angle(degree)
Mθ variation with θ
-3000
-2500
-2000
-1500
-1000
-500
0
500
0 10 20 30 40 50
Nθ(lb/ft)
Angle (degree)
Nθ variation with θ
Beam Theory
Bending Theory
DISCUSSIONS
• The above graphs shows the results obtained from both the theories are quite
close to each other specially for Nx. Mθ, Nθ.
• Nθ Value obtained from beam theory is quite larger than the value obtained
from bending theory.
• The value of Nx obtained from beam theory is lesser at edge of shell and larger
at crown when compared with bending theory.
• The value of Mθ obtained from beam theory is larger at crown compared to
bending theory.
• Nθ value obtained from beam theory is found to be more throughout the shell
except near the crown of shell.
• The value of Q obtained from bending theory is very small
CONCLUSION
• Beam theory being an approximate theory is
quite accurate in determining the forces and
moments in this case.
• Thus the assumption of beam theory to
neglects Q holds good for this long shell.
• Thus the program can be extensively used in
analysing shell very quickly and accurately.
Thank you
References
1. G. S. Ramaswamy, Design and Construction
of Concrete Shell Roofs, McGraw-Hill
Book Co., N.Y., 1968
2. J. E. Gibson, Thin Shell Computation
Theory, Pregmor Press, 1980Science+Business Media. 1992

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Analysis Of Thin Shell

  • 1. ANALYSIS OF SHELL STRUCTURES BY Anik Kumar Mal Meghnad Saha Institute of Technology Department of Civil Engineering Under the guidance of Prof. Dr Bimalendu Ghosh
  • 2. SHELLS Shell Structure in Civil Engineering Construction •The shell structure are very unique due to its interesting strength to weight ratio •They can span over large areas, while having an exceptionally small thickness •Lowers the construction cost •Aesthetic value • Curved structure whose thickness is very less compared to its span. • Depth/Radium < 1/20
  • 4. Analysis of Thin Shell There are mainly 3 Theories- • Bending Theory • Membrane Theory • Approximation Theory
  • 5. Analysis of Thin Shell Bending Theory • This is the most general & accurate theory. • This theory is almost applicable in cases
  • 6. Forces & Moments in Bending Theory: • 6 Unknown Forces: • 4 Unknown Moments:
  • 7. ApproximationTheory, The Beam Theory Advantages- Assumptions: •The deformation of the cross-section in its plane are negligible. •Mx and hence Qx and Mxθ may be ignored. •The strain γxy caused by the shear force Nxθ and the lateral contraction are neglected
  • 8. Analysis By BeamTheory Nx=longitudinal force Nxθ=longitudinally varying shear force Myy=moment about Y axis Iyy= Moment of intertia about Y-axis Q= First static moment about Y Z= depth of neutral axis d=thickness of shell V= shear force Part I
  • 9. AnalysisBy BeamTheory Part II In the 2nd part of analysis the long section of the cylindrical shell have been segmented to number of elementary arches. The main objective of this analysis is to determine Mθ, Nθ
  • 10. Computer Program for Beam Analysis of Cylindrical shell •The program is made in most general way to solve the shell which is applicable for shell of any span and of any radius with any semi- circular angle. •The program is valid for uniformly distributed dead and live load. •The program is applicable for any length of span An analysis of interior shell in a multiple group of shell is done by Beam Theory in book G. Ramaswami. The same problem have been analysed with the program for "interior cylindrical shell analysis in a group of multiple shell" PROBLEM- Geometry span l =62ft Radius a =31ft Thickness d =0.3125ft semicircular angle ф =40° The shell has no edge beam and uniformly loaded. Dead load =47lb/ live load =25lb/( Horizontal projection)
  • 11. Comparison of Result Comparison of Nx degree Angle 0 5 10 15 20 25 30 35 40 lb/ft NX(program) 34099 22392 12058 3178 -4181 -9964 -14127 -16637 -17476 Nx(book) 34145 22421 12074 3183 -4185 -9977 -14144 -16657 -17497 Comparison of Nxθ degree Angle 0 5 10 15 20 25 30 35 40 lb-ft/ft Nxθ(program) 0 4910 7896 9204 9094 7836 5710 3001 0 Nxθ(book) 0 4911 7906 9216 9185 7847 5718 3007 0 Comparison of Mθ degree Angle 0 5 10 15 20 25 30 35 40 lb/ft Mθ(program) -1378 -179.74 477.73 667.03 515.52 172.90 -215.64 -530.7 -694.3 Mθ(book) -1381 -182 475 665 514 173 -215 -526 -687 Comparison of Nθ degree Angle 0 5 10 15 20 25 30 35 40 lb/ft Nθ(progra m) 704.5 7 419.43 -155.50 -873.06 -1606.3 -2251.4 -2728.6 -2983.7 -2989 Nθ(book) 706 420 -156 -875 -1709 -2255 -2733 -2988 -2993 There results obtained from programs are very accurate with less than 1% variation with book
  • 12. Comparison between Beam Theory & Bending Theory A problem of simply supported cylindrical shell analysis is done based on bending theory by following Schorer's approach in book of J. E. Gibson & B. G. Neil PROBLEM Span = 120ft Radius =30ft Semicircular angle =40° load =50lb/ (horizontal projection) Comparison of Nx degree Angle(θ) 0 10 20 30 40 lb/ft NX(beam theory) 86788 30690 -10642 -35955 -44479 Nx(bending theory) 101474 20276 -16684 -29275.8 -31738.3 Comparison of Nxθ degree Angle(θ) 0 10 20 30 40 lb/ft Nxθ(beam theory) 0 10048 11572 7266 0 Nxθ(bending theory) 0 7715.6 7577.6 4256.3 0 Comparison of Mθ degree Angle(θ) 0 10 20 30 40 lb-ft/ft Mθ(beam theory) 0 429.5 1579.6 2826.8 3561.19 Mθ(bending theory) 0 515.2 1718.6 2855.2 3308.7 Comparison of Nθ degree Angle(θ) 0 10 20 30 40 lb/ft Nθ(beam theory) 64 -713.4 -1677.52 -2308.47 -2332.94 Nθ(bending theory) 0 -505.4 -1500.4 -2262.4 -2534.4 Comparison of Q degree Angle(θ) 0 10 20 30 40 lb/ft Q(beam theory) 0 0 0 0 0 Q(bending theory) 0 2.4 3.6 2.7 0
  • 13. -60000 -40000 -20000 0 20000 40000 60000 80000 100000 120000 0 10 20 30 40 50 Nx(lb/ft) Angle(degree) Nx variation with θ 0 2000 4000 6000 8000 10000 12000 14000 0 10 20 30 40 50 Nxθ(lb/ft) Angle (degree) Nxθ variation with θ 0 500 1000 1500 2000 2500 3000 3500 4000 0 10 20 30 40 50 Mθ(lb-ft/ft) angle(degree) Mθ variation with θ -3000 -2500 -2000 -1500 -1000 -500 0 500 0 10 20 30 40 50 Nθ(lb/ft) Angle (degree) Nθ variation with θ Beam Theory Bending Theory
  • 14. DISCUSSIONS • The above graphs shows the results obtained from both the theories are quite close to each other specially for Nx. Mθ, Nθ. • Nθ Value obtained from beam theory is quite larger than the value obtained from bending theory. • The value of Nx obtained from beam theory is lesser at edge of shell and larger at crown when compared with bending theory. • The value of Mθ obtained from beam theory is larger at crown compared to bending theory. • Nθ value obtained from beam theory is found to be more throughout the shell except near the crown of shell. • The value of Q obtained from bending theory is very small
  • 15. CONCLUSION • Beam theory being an approximate theory is quite accurate in determining the forces and moments in this case. • Thus the assumption of beam theory to neglects Q holds good for this long shell. • Thus the program can be extensively used in analysing shell very quickly and accurately.
  • 16. Thank you References 1. G. S. Ramaswamy, Design and Construction of Concrete Shell Roofs, McGraw-Hill Book Co., N.Y., 1968 2. J. E. Gibson, Thin Shell Computation Theory, Pregmor Press, 1980Science+Business Media. 1992