Effect of Load Angle on Limit Load of Polyethylene Miter Pipe Bends 1Source: Journal of Pressure Vessel Technology:;2014:;volume( 136 ):;issue: 003::page 31202DOI: 10.1115/1.4026069Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The aim of this paper is to investigate the effect of crack depth a/W = 0–0.4 and load angle (30 deg, 45 deg, and 60 deg) on the limit load of miter pipe bends (MPB) under outofplane bending moment with a crosshead speed 500 mm/min. The geometry of cracked and uncracked multi miter pipe bends are: bend angle, خ±â€‰= 90 deg, pipe bend factor, h = 0.844, standard dimension ratio, SDR = 11, and three junctions, m = 3. The material of the investigated pipe is a highdensity polyethylene (HDPE), which is applied in natural gas piping systems. Buttfusion welding is used to produce the welds in the miter pipe bends. An artificial crack is produced by a special cracking device. The crack is located at the crown side of the miter pipe bend, such that the crack is collinear with the direction of the applied load. The crack depth ratio, a/W = 0, 0.1, 0.2, 0.3, and 0.4 for outofplane bending moment “i.e., loading angle د• = 0 degâ€. For each outofplane bending moment and all closing and opening load angles the limit load is obtained by the tangent intersection method (TI) from the load deflection curves produced by the specially designed and constructed testing machine at the laboratory (Mechanical Design Department, Faculty of Engineering, Mataria, Helwan University, Cairo/Egypt). For each outofplane bending moment case, the experimental results reveals that increasing crack depth leads to a decrease in the stiffness and limit load of MPB. In case of combined load (outofplane and inplane opening; mode) higher load angles lead to an increase in the limit load. The highest limit load value appears at a loading angle equal, د• = 60 deg. In case of combined load (outofplane and inplane closing; mode) the limit load decreases upon increasing the load angle. On the other hand, higher limit load values appear at a specific loading angle equal د• = 30 deg. For combined load opening case; higher values of limit load are obtained. Contrarily, lower values are obtained in the closing case.
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| contributor author | EL | |
| contributor author | Younan, Maher Y. A. | |
| contributor author | Sallam, Hossam E. M. | |
| contributor author | Abdel | |
| date accessioned | 2017-05-09T01:11:57Z | |
| date available | 2017-05-09T01:11:57Z | |
| date issued | 2014 | |
| identifier issn | 0094-9930 | |
| identifier other | pvt_136_03_031202.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/156132 | |
| description abstract | The aim of this paper is to investigate the effect of crack depth a/W = 0–0.4 and load angle (30 deg, 45 deg, and 60 deg) on the limit load of miter pipe bends (MPB) under outofplane bending moment with a crosshead speed 500 mm/min. The geometry of cracked and uncracked multi miter pipe bends are: bend angle, خ±â€‰= 90 deg, pipe bend factor, h = 0.844, standard dimension ratio, SDR = 11, and three junctions, m = 3. The material of the investigated pipe is a highdensity polyethylene (HDPE), which is applied in natural gas piping systems. Buttfusion welding is used to produce the welds in the miter pipe bends. An artificial crack is produced by a special cracking device. The crack is located at the crown side of the miter pipe bend, such that the crack is collinear with the direction of the applied load. The crack depth ratio, a/W = 0, 0.1, 0.2, 0.3, and 0.4 for outofplane bending moment “i.e., loading angle د• = 0 degâ€. For each outofplane bending moment and all closing and opening load angles the limit load is obtained by the tangent intersection method (TI) from the load deflection curves produced by the specially designed and constructed testing machine at the laboratory (Mechanical Design Department, Faculty of Engineering, Mataria, Helwan University, Cairo/Egypt). For each outofplane bending moment case, the experimental results reveals that increasing crack depth leads to a decrease in the stiffness and limit load of MPB. In case of combined load (outofplane and inplane opening; mode) higher load angles lead to an increase in the limit load. The highest limit load value appears at a loading angle equal, د• = 60 deg. In case of combined load (outofplane and inplane closing; mode) the limit load decreases upon increasing the load angle. On the other hand, higher limit load values appear at a specific loading angle equal د• = 30 deg. For combined load opening case; higher values of limit load are obtained. Contrarily, lower values are obtained in the closing case. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Effect of Load Angle on Limit Load of Polyethylene Miter Pipe Bends 1 | |
| type | Journal Paper | |
| journal volume | 136 | |
| journal issue | 3 | |
| journal title | Journal of Pressure Vessel Technology | |
| identifier doi | 10.1115/1.4026069 | |
| journal fristpage | 31202 | |
| journal lastpage | 31202 | |
| identifier eissn | 1528-8978 | |
| tree | Journal of Pressure Vessel Technology:;2014:;volume( 136 ):;issue: 003 | |
| contenttype | Fulltext |