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International Journal of Trend in Scientific Research and Development (IJTSRD)
Volume 3 Issue 5, August 2019 Available Online: www.ijtsrd.com e-ISSN: 2456 – 6470
@ IJTSRD | Unique Paper ID – IJTSRD27839 | Volume – 3 | Issue – 5 | July - August 2019 Page 2287
Structural Behaviors of Reinforced Concrete Dome with
Shell System under Various Loading Conditions
Khine Zar Aung, Khin Aye Mon, Khin Thanda Htun
Department of Civil Engineering, Yangon Technological University, Yangon, Myanmar
How to cite this paper: Khine Zar Aung |
Khin Aye Mon | Khin Thanda Htun
"Structural Behaviors of Reinforced
Concrete Dome with Shell System under
Various Loading Conditions" Published in
International
Journal of Trend in
Scientific Research
and Development
(ijtsrd), ISSN: 2456-
6470, Volume-3 |
Issue-5, August
2019, pp.2287-
2290,
https://doi.org/10.31142/ijtsrd27839
Copyright © 2019 by author(s) and
International Journal ofTrend inScientific
Research and Development Journal. This
is an Open Access article distributed
under the terms of
the Creative
Commons Attribution
License (CC BY 4.0)
(http://creativecommons.org/licenses/by
/4.0)
ABSTRACT
There are many different systems constructing dome structure. Among them,
the shell system is the most popular in reinforcement concrete structure in
these days. Therefore, it is necessary to know the structural behaviours of it.
The objectives of this journal is to study the structural behaviours of the
reinforced concrete dome structure with shell system under gravity loading
and lateral loading in cyclone wind categories and various seismic zones.
Seismic loads are considered from zone 1 tozone4 based onUBC(1997).Wind
loads are considered from I to V category as cyclone categories. Structural
elements of RC dome structure are designed according to Building Code of
American Concrete Institute (ACI318-99).Withthesememberforces obtained
from the SAP 2000 analysis, the design for all structural members will be
performed according to ACI 318-99. The members of dome structure are
designed as an intermediate moment resisting frame. The design of the shell
beams is verified by using hand calculations with the output forces under the
gravity loading and lateral loading obtained from the SAP2000 analysis.
Equivalent static analysis procedure is used in this study. Based on the
comparison of analysis results, it can be observed where the maximum
deflection occurs along the meridian directionunderseismicandwindloading
conditions. Then, the axial force of dome structureissignificantthananyother
forces in shell system. From the study of analysis results ofbothsystems,ithas
been noticed that the bottom ring in shell system is essential to control the
forces from the shell area.
KEYWORDS: shell system, structural behaviour, seismic loads, wind loads
I. INTRODUCTION
A dome is a self-supporting structural element of
architecture that resembles the hollow upper half of a
sphere. Dome is one of the most efficient shapes intheworld
since it covers the maximum volume with the minimum
surface area. Dome structure can be constructed bydifferent
structural systems. Among them, thin shells with ring beam
as structural elements occupy a leadership position in
engineering. Shell structures support applied externalforces
efficiently by virtue of their geometrical form, as a result,
shells are much stronger and stiffer than other structural
forms [1]. It is light, strong and supported.
II. MODELLING OF REINFORCEDCONCRETE DOME
STRUCTURE
The proposed reinforcedconcretedomestructureis 150 feet
in diameter and 40 feet in height. The thickness of RC dome
is used 6 inches for shell system as shown in Fig.1.There are
four entrances because it is used as sport center. The shell
structural systems constructing in RC dome structure are
considered in this study. This dome structure is designed to
withstand gravity loads, cyclone-level wind loads [2] and
seismic loads from design threats.
The wind loads and seismic loads based on UBC-97 [3] are
assigned to the SAP 2000 model. Wind loads are considered
as cyclone category which intensities are 55.9mph, 77.675
mph, 102 mph, 139.2 mph, 173.4 mph. With these member
forces obtained from the SAP 2000 analysis,thedesignfor all
structural members will be performed accordingtoACI318-
99 [4]. The members of dome structure are designed as an
intermediate moment resistingframe.Thedesignoftheshell
beams is verified by using hand calculations with the output
forces under the gravity loading and lateralloadingobtained
from the SAP2000 analysis.
Fig. 1 Architectural Model of Proposed Dome Structure
IJTSRD27839
International Journal of Trend in Scientific Research and Development (IJTSRD) @ www.ijtsrd.com eISSN: 2456-6470
@ IJTSRD | Unique Paper ID – IJTSRD27839 | Volume – 3 | Issue – 5 | July - August 2019 Page 2288
A. Material properties
Analysis property data,
Weight per unit volume = 150 pcf
Modulus of elasticity = 3605 ksi
Poisson’s ratio = 0 for shell system [4]
Design property data,
Concrete strength (fc') = 4,000 psi
Reinforced yield stress (fy) = 60,000 psi
Shear reinforcing yield stress (fys) = 60,000 psi Data for
dead load
B. Data for gravity load which are used in structural
analysis are as follows:
Superimposed dead load = 20 psf (Ceiling is considered as
superimposed dead loads)
For dome with 1/8 ≤ rise /span ≤3/8, Roof live load =
minimum 16psf (used 20psf).
C. Data for wind load Data for wind load which are
used in structural analysis are as follow:
Exposure type = C
Effective height for wind load = 34 feet
Different wind velocities on model = 55.9mph, 77.675mph,
102mph, 139.2mph, 173.4mph
For slope 2:12 ≤ 4:7.5≤ 9:12,
Windward coefficient Cq= 1.4 for outward due to partially
enclosed structure
Windward coefficient Cq = 0.3 for inward due to partially
enclosed structure
Leeward coefficient = 1.2
Important factor, Iw = 1.0
D. Data for earthquake load
Data for earthquake load which are used in structural
analysis are as follow:
Seismic Zone =1, 2A, 2B, 3 and 4 2B
Zone Factor, Z = 0.075, 0.15,0.2,0.3 and 0.4
Structural System = Shell system
Soil Type = SD
Importance Factor, I = 1
Response Modification Factor, R = 5.5
Seismic Response Coefficient, Ca and Cv are varied according
to the seismic zone and soil profile type.
E. Load Combinations
Design codes applied are ACI 318-99 and UBC-97.There are
26 numbers of load combinations which are accepted in
CQHP (Committee for Quality Control of High-Rise Building
Construction Project).
1. 1.4 DL
2. 1.4 DL + 1.7 LL
3. 1.05 DL+1.275 LL+1.275WX
4. 1.05 DL+1.275 LL-1.275 WX
5. 1.05 DL+1.275 LL+1.275 WY
6. 1.05 DL+1.275 LL-1.275 WY
7. 0.9 DL+1.3WX
8. 0.9 DL-1.3WX
9. 0.9 DL+1.3WY
10. 0.9 DL-1.3WY
11. 0.9 DL+1.02EQX
12. 0.9 DL-1.02EQX
13. 0.9 DL+1.02EQY
14. 0.9 DL-1.02EQY
15. 1.05 DL+1.28LL+EQX
16. 1.05 DL+1.28LL-EQX
17. 1.05 DL+1.28LL+EQY
18. 1.05 DL+1.28LL-EQY
19. 1.16 DL+1.28LL+EQX
20. 1.16 DL+1.28LL-EQX
21. 1.16 DL+1.28LL+EQY
22. 1.16 DL+1.28LL-EQ
23. 0.79 DL+1.02EQX
24. 0.79 DL-1.02EQX
25. 0.79 DL+1.02EQY
26. 0.79DL-1.02EQY
where,
D.L = dead load
L.L = live load
WX = wind load in x direction
WY = wind load in y direction
EQX = earthquake load in x direction
EQY = earthquake load in y direction
III. SHELL BEHAVIORS AND DESIGN
CONSIDERATIONS
While shell system of RC dome structure is analyzed under
gravity loading and lateral loading, membrane actions are
more effected in any other forces in dome structure. Shell
areas are designed under the membrane forces along the
meridian and circumferential directions. In the design of
shell area for dome structure, the reinforcement is placed
due to F11 along circumferential direction and F22 along the
meridian direction. Shear is checked in designed area. The
shear is under the concrete nominal shear.So,itis noneed to
provide shear reinforcement. In design of shell area for RC
dome structure, tensile force can be directly resisted bysteel
and compressive force can be resisted by steel and concrete.
Table1. Provided Steel Areas for Each Portion.
Provided Steel area for
circumferential plane
Provided Steel area for
meridian plane per feet
Top portion No.5 bar @ 6” c/c spacing in
both layer
No.5 bar @ 8’’ c/c spacing in
both layer
Area between openings No.7 bar @ 6’’ c/c spacing in
both layers
No.5 bar @ 6’’ c/c spacing in
both layers
Entrance dome at upper level No.7 bar @ 6’’ c/c spacing in
both layers
No.7 bar @ 6’’ c/c spacing in
both layers
Tension ring at plinth level 6no.9 bars B 24x24
Compression ring at top 3no.5 bars B10x14
International Journal of Trend in Scientific Research and Development (IJTSRD)
@ IJTSRD | Unique Paper ID – IJTSRD27839
Edge beams stiffen the shell edges and act together with the shell in carrying the load of the supporting system. Beam size 2
x24” is used for the edge beam in plinth level. Edge beams carry the longitudinal tensile force. 6No.9 bars are provided for
maximum tensile force Pmax=308 kips.
IV. ANALYSIS RESULTS AND DISCUSSIONS
The gravity loading due to dead load and live load and lateral loading due to wind or earthquake are the major factors that
cause different displacements and forces in reinforced concrete
points on this structure depending on structural configuration as shown in Fig. 2.
Fig.2 The Critical Points of the Plan View of Reinforced Concrete Dome Structure with Shell System
A. Maximum Displacements in Shell System
Fig. 3 shows the maximum displacement in X, Y and Z directions of point 1 which is in middle portion (2) abovewindowunder
twelve critical load combinations. The displacements of X, Y, and Z direction are gradually increased
speed and the seismic zone. The maximum displacement at that point in shell system is 0.26 inches in Z direction which is
under wind load combination 4 (1.05DL+1.275LL
Fig.3 Maximum Displacements at the Point of Middle Po
B. Maximum Membrane Forces of the Shell Area of Bottom Portion
Fig. 4 Maximum membrane forces along the circumferential direction F11 and the meridian direction F22 in the
The Figure 4 shows maximum membrane forces along the circumferential direction F11 and the meridiandirectionF22 inthe
critical area of bottom portion of RC dome with shell system. In critical wind loadingcombination,maximum membranefor
along the circumferential direction F11 and the meridian direction F22 in the critical area of bottom portion are gradually
-0.3
-0.25
-0.2
-0.15
-0.1
-0.05
0
1.4DL
1.4DL+1.7LL
WCOMB(60mph)
WCOMB(80mph)
Displacements(inches)
-250
-200
-150
-100
-50
0
MembraneForces
(kips/ft)
International Journal of Trend in Scientific Research and Development (IJTSRD) @ www.ijtsrd.com
27839 | Volume – 3 | Issue – 5 | July - August 2019
Edge beams stiffen the shell edges and act together with the shell in carrying the load of the supporting system. Beam size 2
x24” is used for the edge beam in plinth level. Edge beams carry the longitudinal tensile force. 6No.9 bars are provided for
ANALYSIS RESULTS AND DISCUSSIONS
The gravity loading due to dead load and live load and lateral loading due to wind or earthquake are the major factors that
cause different displacements and forces in reinforced concrete dome structure with shell system.
depending on structural configuration as shown in Fig. 2.
Fig.2 The Critical Points of the Plan View of Reinforced Concrete Dome Structure with Shell System
Displacements in Shell System
Fig. 3 shows the maximum displacement in X, Y and Z directions of point 1 which is in middle portion (2) abovewindowunder
twelve critical load combinations. The displacements of X, Y, and Z direction are gradually increased
speed and the seismic zone. The maximum displacement at that point in shell system is 0.26 inches in Z direction which is
combination 4 (1.05DL+1.275LL-1.275WX).
Fig.3 Maximum Displacements at the Point of Middle Portion (2) above Window in Shell System of Dome
Maximum Membrane Forces of the Shell Area of Bottom Portion
Fig. 4 Maximum membrane forces along the circumferential direction F11 and the meridian direction F22 in the
critical area of bottom
The Figure 4 shows maximum membrane forces along the circumferential direction F11 and the meridiandirectionF22 inthe
critical area of bottom portion of RC dome with shell system. In critical wind loadingcombination,maximum membranefor
along the circumferential direction F11 and the meridian direction F22 in the critical area of bottom portion are gradually
WCOMB(100mph)
WCOMB(140mph)
WCOMB(175mph)
EQCOMBZONE1
EQCOMBZONE2A
EQCOMBZONE2B
EQCOMBZONE3
EQCOMBZONE4
At point 2, Max displacement
U1 in X direction (inches)
At point 2, Max displacement
U2 in Y direction (inches)
At point 2, Max displacement
U3 in Z direction (inches)
Forces along circumferential
direction F11 (kip/ft)
Forces along meridian
direction F22 (kip/ft)
www.ijtsrd.com eISSN: 2456-6470
August 2019 Page 2289
Edge beams stiffen the shell edges and act together with the shell in carrying the load of the supporting system. Beam size 24”
x24” is used for the edge beam in plinth level. Edge beams carry the longitudinal tensile force. 6No.9 bars are provided for
The gravity loading due to dead load and live load and lateral loading due to wind or earthquake are the major factors that
dome structure with shell system. There are seven critical
Fig.2 The Critical Points of the Plan View of Reinforced Concrete Dome Structure with Shell System
Fig. 3 shows the maximum displacement in X, Y and Z directions of point 1 which is in middle portion (2) abovewindowunder
twelve critical load combinations. The displacements of X, Y, and Z direction are gradually increased according to the wind
speed and the seismic zone. The maximum displacement at that point in shell system is 0.26 inches in Z direction which is
rtion (2) above Window in Shell System of Dome
Fig. 4 Maximum membrane forces along the circumferential direction F11 and the meridian direction F22 in the
The Figure 4 shows maximum membrane forces along the circumferential direction F11 and the meridiandirectionF22 inthe
critical area of bottom portion of RC dome with shell system. In critical wind loadingcombination,maximum membraneforces
along the circumferential direction F11 and the meridian direction F22 in the critical area of bottom portion are gradually
At point 2, Max displacement
U1 in X direction (inches)
At point 2, Max displacement
U2 in Y direction (inches)
At point 2, Max displacement
U3 in Z direction (inches)
Forces along circumferential
direction F11 (kip/ft)
Forces along meridian
direction F22 (kip/ft)
International Journal of Trend in Scientific Research and Development (IJTSRD) @ www.ijtsrd.com eISSN: 2456-6470
@ IJTSRD | Unique Paper ID – IJTSRD27839 | Volume – 3 | Issue – 5 | July - August 2019 Page 2290
increased according to the wind speed and that of under seismic load combinations are also graduallyincreasedas theseismic
zone is high. The maximum membrane force along the meridian direction F22 in the critical area of bottom portion under
maximum wind loading is more than that under gravity loading and maximum seismic loading combination by1.12times and
1.34 times.
C. Maximum Forces of Critical Ring Beams in Shell System
Fig. 5 shows the critical axial force, major shear, minor shear, major bending moment, and torsional moment of the critical
bottom ring beam (8) in shell system under twelve critical load combinations. Among them, the axial force and bending
moment are the significant forces under all critical loading. The maximum axial force in the critical bottom ring beam I inshell
system is 200.4 kips which is under wind load combination4 (1.05DL+1.275LL-1.275WX).
Fig.5 Critical Forces of Critical Bottom Ring Beam (8) in Shell System
D. Critical Reactions of the Shell System
Fig.6 Maximum Reactions F1 in X Direction, F2 in Y Direction, and F3 in Z Direction at Critical Point (9) at the Base
of Y Beam in Shell System
Fig. 6 shows the reactions F1 in X direction, F2 in Y direction, and F3 in Z direction at the critical point (9) at the base ofYbeam
in shell system under twelve critical load combinations. The reactions ofX,Y,andZ directionaregradually increasedaccording
to wind speed and seismic zone. The maximum reactions in shell system is 207 kips in Z direction which is under wind load
combination 4 (1.05DL+1.275LL-1.275WX).
V. CONCLUSION
From the above study, it can be concluded as the following.
1. From the study of analysis results of shell system in RC
dome, the maximum displacement occurs in Z direction
in the middle portion of dome under wind load
combination.
2. The membrane forces arealsothemaximumunderwind
load combination in both meridian and circumferential
directions.
3. From the analysis result of critical bottom ring beam,
the axial forces are 230 kips in shell system. Therefore,
the bottom ring in shell system of dome structure is
essential to control the forces from the shell area.
4. The critical reaction in Z direction is control any other
reactions in shell system. The maximum reaction in this
system of dome is 207 kips which is also under windthe
combination.
ACKNOWLEDGEMENTS
The authors are extremely grateful to the teachers from
Department of Civil Engineering in Yangon Technological
University, for their guidance, advice and encourages for
completing this paper.
REFERENCES
[1]. Aduard Ventsel, Theodor Krauthammer. 2001. Thin
Plate and Shell, The Pennsylvania State University,
University Park, Pennsylvania
[2]. National Weather Service (NOAA). No Date. ‘‘Saffir-
Simpson Hurricane Scale’’, August 2012 < http://
www.ohesp.lousiana.gov/hurricanecategories.htm>
[3]. International Conference of Building Officials. 1997.
Structural Engineering Design Provisions, Uniform
Building Code. Volume 2.
[4]. American Concrete Institute Committee.1999.Building
Code Requirements for Structural Concrete and
Commentary ( ACI318.99 ). U.S.A American Concrete
Institute Committee
-150
-100
-50
0
50
100
150
200
250
1.4DL
1.4DL+1.7LL
WCOMB(60
mph)
WCOMB(80
mph)
WCOMB(100
mph)
WCOMB(140
mph)
WCOMB
(175mph)
EQCOMBZONE
1
EQCOMBZONE
2A
EQCOMBZONE
2B
EQCOMBZONE
3
EQCOMBZONE
4
forces
At critical bottom ring beam (8) critical
axial force P (kip)
At critical bottom ring beam (8) Critical
major bending moment M3 (kip-ft)
At critical bottom ring beam (8) Critical
shear force v2 (kip)
At critical bottom ring beam (8) Critical
shear force v3 (kip)
At critical bottom ring beam (8) Critical
torsional moment M3 (kip-ft)
-50
0
50
100
150
200
250
Reaction in X direction F1 (kips)
Reaction in Y direction F2 (kips)
Reaction in Z direction F3 (kips)
Reactions(kips)

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Structural Behaviors of Reinforced Concrete Dome with Shell System under Various Loading Conditions

  • 1. International Journal of Trend in Scientific Research and Development (IJTSRD) Volume 3 Issue 5, August 2019 Available Online: www.ijtsrd.com e-ISSN: 2456 – 6470 @ IJTSRD | Unique Paper ID – IJTSRD27839 | Volume – 3 | Issue – 5 | July - August 2019 Page 2287 Structural Behaviors of Reinforced Concrete Dome with Shell System under Various Loading Conditions Khine Zar Aung, Khin Aye Mon, Khin Thanda Htun Department of Civil Engineering, Yangon Technological University, Yangon, Myanmar How to cite this paper: Khine Zar Aung | Khin Aye Mon | Khin Thanda Htun "Structural Behaviors of Reinforced Concrete Dome with Shell System under Various Loading Conditions" Published in International Journal of Trend in Scientific Research and Development (ijtsrd), ISSN: 2456- 6470, Volume-3 | Issue-5, August 2019, pp.2287- 2290, https://doi.org/10.31142/ijtsrd27839 Copyright © 2019 by author(s) and International Journal ofTrend inScientific Research and Development Journal. This is an Open Access article distributed under the terms of the Creative Commons Attribution License (CC BY 4.0) (http://creativecommons.org/licenses/by /4.0) ABSTRACT There are many different systems constructing dome structure. Among them, the shell system is the most popular in reinforcement concrete structure in these days. Therefore, it is necessary to know the structural behaviours of it. The objectives of this journal is to study the structural behaviours of the reinforced concrete dome structure with shell system under gravity loading and lateral loading in cyclone wind categories and various seismic zones. Seismic loads are considered from zone 1 tozone4 based onUBC(1997).Wind loads are considered from I to V category as cyclone categories. Structural elements of RC dome structure are designed according to Building Code of American Concrete Institute (ACI318-99).Withthesememberforces obtained from the SAP 2000 analysis, the design for all structural members will be performed according to ACI 318-99. The members of dome structure are designed as an intermediate moment resisting frame. The design of the shell beams is verified by using hand calculations with the output forces under the gravity loading and lateral loading obtained from the SAP2000 analysis. Equivalent static analysis procedure is used in this study. Based on the comparison of analysis results, it can be observed where the maximum deflection occurs along the meridian directionunderseismicandwindloading conditions. Then, the axial force of dome structureissignificantthananyother forces in shell system. From the study of analysis results ofbothsystems,ithas been noticed that the bottom ring in shell system is essential to control the forces from the shell area. KEYWORDS: shell system, structural behaviour, seismic loads, wind loads I. INTRODUCTION A dome is a self-supporting structural element of architecture that resembles the hollow upper half of a sphere. Dome is one of the most efficient shapes intheworld since it covers the maximum volume with the minimum surface area. Dome structure can be constructed bydifferent structural systems. Among them, thin shells with ring beam as structural elements occupy a leadership position in engineering. Shell structures support applied externalforces efficiently by virtue of their geometrical form, as a result, shells are much stronger and stiffer than other structural forms [1]. It is light, strong and supported. II. MODELLING OF REINFORCEDCONCRETE DOME STRUCTURE The proposed reinforcedconcretedomestructureis 150 feet in diameter and 40 feet in height. The thickness of RC dome is used 6 inches for shell system as shown in Fig.1.There are four entrances because it is used as sport center. The shell structural systems constructing in RC dome structure are considered in this study. This dome structure is designed to withstand gravity loads, cyclone-level wind loads [2] and seismic loads from design threats. The wind loads and seismic loads based on UBC-97 [3] are assigned to the SAP 2000 model. Wind loads are considered as cyclone category which intensities are 55.9mph, 77.675 mph, 102 mph, 139.2 mph, 173.4 mph. With these member forces obtained from the SAP 2000 analysis,thedesignfor all structural members will be performed accordingtoACI318- 99 [4]. The members of dome structure are designed as an intermediate moment resistingframe.Thedesignoftheshell beams is verified by using hand calculations with the output forces under the gravity loading and lateralloadingobtained from the SAP2000 analysis. Fig. 1 Architectural Model of Proposed Dome Structure IJTSRD27839
  • 2. International Journal of Trend in Scientific Research and Development (IJTSRD) @ www.ijtsrd.com eISSN: 2456-6470 @ IJTSRD | Unique Paper ID – IJTSRD27839 | Volume – 3 | Issue – 5 | July - August 2019 Page 2288 A. Material properties Analysis property data, Weight per unit volume = 150 pcf Modulus of elasticity = 3605 ksi Poisson’s ratio = 0 for shell system [4] Design property data, Concrete strength (fc') = 4,000 psi Reinforced yield stress (fy) = 60,000 psi Shear reinforcing yield stress (fys) = 60,000 psi Data for dead load B. Data for gravity load which are used in structural analysis are as follows: Superimposed dead load = 20 psf (Ceiling is considered as superimposed dead loads) For dome with 1/8 ≤ rise /span ≤3/8, Roof live load = minimum 16psf (used 20psf). C. Data for wind load Data for wind load which are used in structural analysis are as follow: Exposure type = C Effective height for wind load = 34 feet Different wind velocities on model = 55.9mph, 77.675mph, 102mph, 139.2mph, 173.4mph For slope 2:12 ≤ 4:7.5≤ 9:12, Windward coefficient Cq= 1.4 for outward due to partially enclosed structure Windward coefficient Cq = 0.3 for inward due to partially enclosed structure Leeward coefficient = 1.2 Important factor, Iw = 1.0 D. Data for earthquake load Data for earthquake load which are used in structural analysis are as follow: Seismic Zone =1, 2A, 2B, 3 and 4 2B Zone Factor, Z = 0.075, 0.15,0.2,0.3 and 0.4 Structural System = Shell system Soil Type = SD Importance Factor, I = 1 Response Modification Factor, R = 5.5 Seismic Response Coefficient, Ca and Cv are varied according to the seismic zone and soil profile type. E. Load Combinations Design codes applied are ACI 318-99 and UBC-97.There are 26 numbers of load combinations which are accepted in CQHP (Committee for Quality Control of High-Rise Building Construction Project). 1. 1.4 DL 2. 1.4 DL + 1.7 LL 3. 1.05 DL+1.275 LL+1.275WX 4. 1.05 DL+1.275 LL-1.275 WX 5. 1.05 DL+1.275 LL+1.275 WY 6. 1.05 DL+1.275 LL-1.275 WY 7. 0.9 DL+1.3WX 8. 0.9 DL-1.3WX 9. 0.9 DL+1.3WY 10. 0.9 DL-1.3WY 11. 0.9 DL+1.02EQX 12. 0.9 DL-1.02EQX 13. 0.9 DL+1.02EQY 14. 0.9 DL-1.02EQY 15. 1.05 DL+1.28LL+EQX 16. 1.05 DL+1.28LL-EQX 17. 1.05 DL+1.28LL+EQY 18. 1.05 DL+1.28LL-EQY 19. 1.16 DL+1.28LL+EQX 20. 1.16 DL+1.28LL-EQX 21. 1.16 DL+1.28LL+EQY 22. 1.16 DL+1.28LL-EQ 23. 0.79 DL+1.02EQX 24. 0.79 DL-1.02EQX 25. 0.79 DL+1.02EQY 26. 0.79DL-1.02EQY where, D.L = dead load L.L = live load WX = wind load in x direction WY = wind load in y direction EQX = earthquake load in x direction EQY = earthquake load in y direction III. SHELL BEHAVIORS AND DESIGN CONSIDERATIONS While shell system of RC dome structure is analyzed under gravity loading and lateral loading, membrane actions are more effected in any other forces in dome structure. Shell areas are designed under the membrane forces along the meridian and circumferential directions. In the design of shell area for dome structure, the reinforcement is placed due to F11 along circumferential direction and F22 along the meridian direction. Shear is checked in designed area. The shear is under the concrete nominal shear.So,itis noneed to provide shear reinforcement. In design of shell area for RC dome structure, tensile force can be directly resisted bysteel and compressive force can be resisted by steel and concrete. Table1. Provided Steel Areas for Each Portion. Provided Steel area for circumferential plane Provided Steel area for meridian plane per feet Top portion No.5 bar @ 6” c/c spacing in both layer No.5 bar @ 8’’ c/c spacing in both layer Area between openings No.7 bar @ 6’’ c/c spacing in both layers No.5 bar @ 6’’ c/c spacing in both layers Entrance dome at upper level No.7 bar @ 6’’ c/c spacing in both layers No.7 bar @ 6’’ c/c spacing in both layers Tension ring at plinth level 6no.9 bars B 24x24 Compression ring at top 3no.5 bars B10x14
  • 3. International Journal of Trend in Scientific Research and Development (IJTSRD) @ IJTSRD | Unique Paper ID – IJTSRD27839 Edge beams stiffen the shell edges and act together with the shell in carrying the load of the supporting system. Beam size 2 x24” is used for the edge beam in plinth level. Edge beams carry the longitudinal tensile force. 6No.9 bars are provided for maximum tensile force Pmax=308 kips. IV. ANALYSIS RESULTS AND DISCUSSIONS The gravity loading due to dead load and live load and lateral loading due to wind or earthquake are the major factors that cause different displacements and forces in reinforced concrete points on this structure depending on structural configuration as shown in Fig. 2. Fig.2 The Critical Points of the Plan View of Reinforced Concrete Dome Structure with Shell System A. Maximum Displacements in Shell System Fig. 3 shows the maximum displacement in X, Y and Z directions of point 1 which is in middle portion (2) abovewindowunder twelve critical load combinations. The displacements of X, Y, and Z direction are gradually increased speed and the seismic zone. The maximum displacement at that point in shell system is 0.26 inches in Z direction which is under wind load combination 4 (1.05DL+1.275LL Fig.3 Maximum Displacements at the Point of Middle Po B. Maximum Membrane Forces of the Shell Area of Bottom Portion Fig. 4 Maximum membrane forces along the circumferential direction F11 and the meridian direction F22 in the The Figure 4 shows maximum membrane forces along the circumferential direction F11 and the meridiandirectionF22 inthe critical area of bottom portion of RC dome with shell system. In critical wind loadingcombination,maximum membranefor along the circumferential direction F11 and the meridian direction F22 in the critical area of bottom portion are gradually -0.3 -0.25 -0.2 -0.15 -0.1 -0.05 0 1.4DL 1.4DL+1.7LL WCOMB(60mph) WCOMB(80mph) Displacements(inches) -250 -200 -150 -100 -50 0 MembraneForces (kips/ft) International Journal of Trend in Scientific Research and Development (IJTSRD) @ www.ijtsrd.com 27839 | Volume – 3 | Issue – 5 | July - August 2019 Edge beams stiffen the shell edges and act together with the shell in carrying the load of the supporting system. Beam size 2 x24” is used for the edge beam in plinth level. Edge beams carry the longitudinal tensile force. 6No.9 bars are provided for ANALYSIS RESULTS AND DISCUSSIONS The gravity loading due to dead load and live load and lateral loading due to wind or earthquake are the major factors that cause different displacements and forces in reinforced concrete dome structure with shell system. depending on structural configuration as shown in Fig. 2. Fig.2 The Critical Points of the Plan View of Reinforced Concrete Dome Structure with Shell System Displacements in Shell System Fig. 3 shows the maximum displacement in X, Y and Z directions of point 1 which is in middle portion (2) abovewindowunder twelve critical load combinations. The displacements of X, Y, and Z direction are gradually increased speed and the seismic zone. The maximum displacement at that point in shell system is 0.26 inches in Z direction which is combination 4 (1.05DL+1.275LL-1.275WX). Fig.3 Maximum Displacements at the Point of Middle Portion (2) above Window in Shell System of Dome Maximum Membrane Forces of the Shell Area of Bottom Portion Fig. 4 Maximum membrane forces along the circumferential direction F11 and the meridian direction F22 in the critical area of bottom The Figure 4 shows maximum membrane forces along the circumferential direction F11 and the meridiandirectionF22 inthe critical area of bottom portion of RC dome with shell system. In critical wind loadingcombination,maximum membranefor along the circumferential direction F11 and the meridian direction F22 in the critical area of bottom portion are gradually WCOMB(100mph) WCOMB(140mph) WCOMB(175mph) EQCOMBZONE1 EQCOMBZONE2A EQCOMBZONE2B EQCOMBZONE3 EQCOMBZONE4 At point 2, Max displacement U1 in X direction (inches) At point 2, Max displacement U2 in Y direction (inches) At point 2, Max displacement U3 in Z direction (inches) Forces along circumferential direction F11 (kip/ft) Forces along meridian direction F22 (kip/ft) www.ijtsrd.com eISSN: 2456-6470 August 2019 Page 2289 Edge beams stiffen the shell edges and act together with the shell in carrying the load of the supporting system. Beam size 24” x24” is used for the edge beam in plinth level. Edge beams carry the longitudinal tensile force. 6No.9 bars are provided for The gravity loading due to dead load and live load and lateral loading due to wind or earthquake are the major factors that dome structure with shell system. There are seven critical Fig.2 The Critical Points of the Plan View of Reinforced Concrete Dome Structure with Shell System Fig. 3 shows the maximum displacement in X, Y and Z directions of point 1 which is in middle portion (2) abovewindowunder twelve critical load combinations. The displacements of X, Y, and Z direction are gradually increased according to the wind speed and the seismic zone. The maximum displacement at that point in shell system is 0.26 inches in Z direction which is rtion (2) above Window in Shell System of Dome Fig. 4 Maximum membrane forces along the circumferential direction F11 and the meridian direction F22 in the The Figure 4 shows maximum membrane forces along the circumferential direction F11 and the meridiandirectionF22 inthe critical area of bottom portion of RC dome with shell system. In critical wind loadingcombination,maximum membraneforces along the circumferential direction F11 and the meridian direction F22 in the critical area of bottom portion are gradually At point 2, Max displacement U1 in X direction (inches) At point 2, Max displacement U2 in Y direction (inches) At point 2, Max displacement U3 in Z direction (inches) Forces along circumferential direction F11 (kip/ft) Forces along meridian direction F22 (kip/ft)
  • 4. International Journal of Trend in Scientific Research and Development (IJTSRD) @ www.ijtsrd.com eISSN: 2456-6470 @ IJTSRD | Unique Paper ID – IJTSRD27839 | Volume – 3 | Issue – 5 | July - August 2019 Page 2290 increased according to the wind speed and that of under seismic load combinations are also graduallyincreasedas theseismic zone is high. The maximum membrane force along the meridian direction F22 in the critical area of bottom portion under maximum wind loading is more than that under gravity loading and maximum seismic loading combination by1.12times and 1.34 times. C. Maximum Forces of Critical Ring Beams in Shell System Fig. 5 shows the critical axial force, major shear, minor shear, major bending moment, and torsional moment of the critical bottom ring beam (8) in shell system under twelve critical load combinations. Among them, the axial force and bending moment are the significant forces under all critical loading. The maximum axial force in the critical bottom ring beam I inshell system is 200.4 kips which is under wind load combination4 (1.05DL+1.275LL-1.275WX). Fig.5 Critical Forces of Critical Bottom Ring Beam (8) in Shell System D. Critical Reactions of the Shell System Fig.6 Maximum Reactions F1 in X Direction, F2 in Y Direction, and F3 in Z Direction at Critical Point (9) at the Base of Y Beam in Shell System Fig. 6 shows the reactions F1 in X direction, F2 in Y direction, and F3 in Z direction at the critical point (9) at the base ofYbeam in shell system under twelve critical load combinations. The reactions ofX,Y,andZ directionaregradually increasedaccording to wind speed and seismic zone. The maximum reactions in shell system is 207 kips in Z direction which is under wind load combination 4 (1.05DL+1.275LL-1.275WX). V. CONCLUSION From the above study, it can be concluded as the following. 1. From the study of analysis results of shell system in RC dome, the maximum displacement occurs in Z direction in the middle portion of dome under wind load combination. 2. The membrane forces arealsothemaximumunderwind load combination in both meridian and circumferential directions. 3. From the analysis result of critical bottom ring beam, the axial forces are 230 kips in shell system. Therefore, the bottom ring in shell system of dome structure is essential to control the forces from the shell area. 4. The critical reaction in Z direction is control any other reactions in shell system. The maximum reaction in this system of dome is 207 kips which is also under windthe combination. ACKNOWLEDGEMENTS The authors are extremely grateful to the teachers from Department of Civil Engineering in Yangon Technological University, for their guidance, advice and encourages for completing this paper. REFERENCES [1]. Aduard Ventsel, Theodor Krauthammer. 2001. Thin Plate and Shell, The Pennsylvania State University, University Park, Pennsylvania [2]. National Weather Service (NOAA). No Date. ‘‘Saffir- Simpson Hurricane Scale’’, August 2012 < http:// www.ohesp.lousiana.gov/hurricanecategories.htm> [3]. International Conference of Building Officials. 1997. Structural Engineering Design Provisions, Uniform Building Code. Volume 2. [4]. American Concrete Institute Committee.1999.Building Code Requirements for Structural Concrete and Commentary ( ACI318.99 ). U.S.A American Concrete Institute Committee -150 -100 -50 0 50 100 150 200 250 1.4DL 1.4DL+1.7LL WCOMB(60 mph) WCOMB(80 mph) WCOMB(100 mph) WCOMB(140 mph) WCOMB (175mph) EQCOMBZONE 1 EQCOMBZONE 2A EQCOMBZONE 2B EQCOMBZONE 3 EQCOMBZONE 4 forces At critical bottom ring beam (8) critical axial force P (kip) At critical bottom ring beam (8) Critical major bending moment M3 (kip-ft) At critical bottom ring beam (8) Critical shear force v2 (kip) At critical bottom ring beam (8) Critical shear force v3 (kip) At critical bottom ring beam (8) Critical torsional moment M3 (kip-ft) -50 0 50 100 150 200 250 Reaction in X direction F1 (kips) Reaction in Y direction F2 (kips) Reaction in Z direction F3 (kips) Reactions(kips)