On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit
Abstract The basic nonlinear relations describing the stress-strain state of flexible thin-walled elements (rods, rings) that stiffen the contour of curvilinear openings in shells with allowance for the plastic deformation of their materials are presented. The Lagrange variation equation is used to...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Mulyar, V. P. [verfasserIn] Storozhuk, E. A. [verfasserIn] Chernyshenko, I. S. [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
1999 |
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| Schlagwörter: |
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| Übergeordnetes Werk: |
Enthalten in: International applied mechanics - New York, NY [u.a.] : Consultants Bureau, 1966, 35(1999), 5 vom: Mai, Seite 508-514 |
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| Übergeordnetes Werk: |
volume:35 ; year:1999 ; number:5 ; month:05 ; pages:508-514 |
| Links: |
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| DOI / URN: |
10.1007/BF03355411 |
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| Katalog-ID: |
SPR013197401 |
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| 100 | 1 | |a Mulyar, V. P. |e verfasserin |4 aut | |
| 245 | 1 | 0 | |a On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit |
| 264 | 1 | |c 1999 | |
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| 520 | |a Abstract The basic nonlinear relations describing the stress-strain state of flexible thin-walled elements (rods, rings) that stiffen the contour of curvilinear openings in shells with allowance for the plastic deformation of their materials are presented. The Lagrange variation equation is used to obtain sets of nonlinear resolving equations for a shell with a stiffened elliptical opening. Successive-approximation and finite-element methods are used to solve the nonlinear problems. Numerical results are given for an elastoplastic cylindrical shell loaded by an internal pressure of given intensity. The distribution of maximum stresses in the area of an elliptical opening with and without a stiffening ring is analyzed. The data obtained in elastoplastic and linearly elastic formulations of the problem are compared. | ||
| 650 | 4 | |a Cylindrical Shell |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Internal Pressure |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Spherical Shell |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Elliptical Opening |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Nonlinear Deformation |7 (dpeaa)DE-He213 | |
| 700 | 1 | |a Storozhuk, E. A. |e verfasserin |4 aut | |
| 700 | 1 | |a Chernyshenko, I. S. |e verfasserin |4 aut | |
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| 773 | 1 | 8 | |g volume:35 |g year:1999 |g number:5 |g month:05 |g pages:508-514 |
| 856 | 4 | 0 | |u https://dx.doi.org/10.1007/BF03355411 |z lizenzpflichtig |3 Volltext |
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10.1007/BF03355411 doi (DE-627)SPR013197401 (SPR)BF03355411-e DE-627 ger DE-627 rakwb eng 530 ASE 50.31 bkl Mulyar, V. P. verfasserin aut On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit 1999 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The basic nonlinear relations describing the stress-strain state of flexible thin-walled elements (rods, rings) that stiffen the contour of curvilinear openings in shells with allowance for the plastic deformation of their materials are presented. The Lagrange variation equation is used to obtain sets of nonlinear resolving equations for a shell with a stiffened elliptical opening. Successive-approximation and finite-element methods are used to solve the nonlinear problems. Numerical results are given for an elastoplastic cylindrical shell loaded by an internal pressure of given intensity. The distribution of maximum stresses in the area of an elliptical opening with and without a stiffening ring is analyzed. The data obtained in elastoplastic and linearly elastic formulations of the problem are compared. Cylindrical Shell (dpeaa)DE-He213 Internal Pressure (dpeaa)DE-He213 Spherical Shell (dpeaa)DE-He213 Elliptical Opening (dpeaa)DE-He213 Nonlinear Deformation (dpeaa)DE-He213 Storozhuk, E. A. verfasserin aut Chernyshenko, I. S. verfasserin aut Enthalten in International applied mechanics New York, NY [u.a.] : Consultants Bureau, 1966 35(1999), 5 vom: Mai, Seite 508-514 (DE-627)32557040X (DE-600)2037331-4 1573-8582 nnns volume:35 year:1999 number:5 month:05 pages:508-514 https://dx.doi.org/10.1007/BF03355411 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_121 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_374 GBV_ILN_602 GBV_ILN_636 GBV_ILN_647 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2018 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2043 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2158 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2193 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_2808 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4277 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4346 GBV_ILN_4367 GBV_ILN_4393 GBV_ILN_4700 GBV_ILN_4753 50.31 ASE AR 35 1999 5 05 508-514 |
| spelling |
10.1007/BF03355411 doi (DE-627)SPR013197401 (SPR)BF03355411-e DE-627 ger DE-627 rakwb eng 530 ASE 50.31 bkl Mulyar, V. P. verfasserin aut On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit 1999 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The basic nonlinear relations describing the stress-strain state of flexible thin-walled elements (rods, rings) that stiffen the contour of curvilinear openings in shells with allowance for the plastic deformation of their materials are presented. The Lagrange variation equation is used to obtain sets of nonlinear resolving equations for a shell with a stiffened elliptical opening. Successive-approximation and finite-element methods are used to solve the nonlinear problems. Numerical results are given for an elastoplastic cylindrical shell loaded by an internal pressure of given intensity. The distribution of maximum stresses in the area of an elliptical opening with and without a stiffening ring is analyzed. The data obtained in elastoplastic and linearly elastic formulations of the problem are compared. Cylindrical Shell (dpeaa)DE-He213 Internal Pressure (dpeaa)DE-He213 Spherical Shell (dpeaa)DE-He213 Elliptical Opening (dpeaa)DE-He213 Nonlinear Deformation (dpeaa)DE-He213 Storozhuk, E. A. verfasserin aut Chernyshenko, I. S. verfasserin aut Enthalten in International applied mechanics New York, NY [u.a.] : Consultants Bureau, 1966 35(1999), 5 vom: Mai, Seite 508-514 (DE-627)32557040X (DE-600)2037331-4 1573-8582 nnns volume:35 year:1999 number:5 month:05 pages:508-514 https://dx.doi.org/10.1007/BF03355411 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_121 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_374 GBV_ILN_602 GBV_ILN_636 GBV_ILN_647 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2018 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2043 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2158 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2193 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_2808 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4277 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4346 GBV_ILN_4367 GBV_ILN_4393 GBV_ILN_4700 GBV_ILN_4753 50.31 ASE AR 35 1999 5 05 508-514 |
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10.1007/BF03355411 doi (DE-627)SPR013197401 (SPR)BF03355411-e DE-627 ger DE-627 rakwb eng 530 ASE 50.31 bkl Mulyar, V. P. verfasserin aut On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit 1999 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The basic nonlinear relations describing the stress-strain state of flexible thin-walled elements (rods, rings) that stiffen the contour of curvilinear openings in shells with allowance for the plastic deformation of their materials are presented. The Lagrange variation equation is used to obtain sets of nonlinear resolving equations for a shell with a stiffened elliptical opening. Successive-approximation and finite-element methods are used to solve the nonlinear problems. Numerical results are given for an elastoplastic cylindrical shell loaded by an internal pressure of given intensity. The distribution of maximum stresses in the area of an elliptical opening with and without a stiffening ring is analyzed. The data obtained in elastoplastic and linearly elastic formulations of the problem are compared. Cylindrical Shell (dpeaa)DE-He213 Internal Pressure (dpeaa)DE-He213 Spherical Shell (dpeaa)DE-He213 Elliptical Opening (dpeaa)DE-He213 Nonlinear Deformation (dpeaa)DE-He213 Storozhuk, E. A. verfasserin aut Chernyshenko, I. S. verfasserin aut Enthalten in International applied mechanics New York, NY [u.a.] : Consultants Bureau, 1966 35(1999), 5 vom: Mai, Seite 508-514 (DE-627)32557040X (DE-600)2037331-4 1573-8582 nnns volume:35 year:1999 number:5 month:05 pages:508-514 https://dx.doi.org/10.1007/BF03355411 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_121 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_374 GBV_ILN_602 GBV_ILN_636 GBV_ILN_647 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2018 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2043 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2158 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2193 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_2808 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4277 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4346 GBV_ILN_4367 GBV_ILN_4393 GBV_ILN_4700 GBV_ILN_4753 50.31 ASE AR 35 1999 5 05 508-514 |
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10.1007/BF03355411 doi (DE-627)SPR013197401 (SPR)BF03355411-e DE-627 ger DE-627 rakwb eng 530 ASE 50.31 bkl Mulyar, V. P. verfasserin aut On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit 1999 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The basic nonlinear relations describing the stress-strain state of flexible thin-walled elements (rods, rings) that stiffen the contour of curvilinear openings in shells with allowance for the plastic deformation of their materials are presented. The Lagrange variation equation is used to obtain sets of nonlinear resolving equations for a shell with a stiffened elliptical opening. Successive-approximation and finite-element methods are used to solve the nonlinear problems. Numerical results are given for an elastoplastic cylindrical shell loaded by an internal pressure of given intensity. The distribution of maximum stresses in the area of an elliptical opening with and without a stiffening ring is analyzed. The data obtained in elastoplastic and linearly elastic formulations of the problem are compared. Cylindrical Shell (dpeaa)DE-He213 Internal Pressure (dpeaa)DE-He213 Spherical Shell (dpeaa)DE-He213 Elliptical Opening (dpeaa)DE-He213 Nonlinear Deformation (dpeaa)DE-He213 Storozhuk, E. A. verfasserin aut Chernyshenko, I. S. verfasserin aut Enthalten in International applied mechanics New York, NY [u.a.] : Consultants Bureau, 1966 35(1999), 5 vom: Mai, Seite 508-514 (DE-627)32557040X (DE-600)2037331-4 1573-8582 nnns volume:35 year:1999 number:5 month:05 pages:508-514 https://dx.doi.org/10.1007/BF03355411 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_121 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_374 GBV_ILN_602 GBV_ILN_636 GBV_ILN_647 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2018 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2043 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2158 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2193 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_2808 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4277 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4346 GBV_ILN_4367 GBV_ILN_4393 GBV_ILN_4700 GBV_ILN_4753 50.31 ASE AR 35 1999 5 05 508-514 |
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10.1007/BF03355411 doi (DE-627)SPR013197401 (SPR)BF03355411-e DE-627 ger DE-627 rakwb eng 530 ASE 50.31 bkl Mulyar, V. P. verfasserin aut On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit 1999 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The basic nonlinear relations describing the stress-strain state of flexible thin-walled elements (rods, rings) that stiffen the contour of curvilinear openings in shells with allowance for the plastic deformation of their materials are presented. The Lagrange variation equation is used to obtain sets of nonlinear resolving equations for a shell with a stiffened elliptical opening. Successive-approximation and finite-element methods are used to solve the nonlinear problems. Numerical results are given for an elastoplastic cylindrical shell loaded by an internal pressure of given intensity. The distribution of maximum stresses in the area of an elliptical opening with and without a stiffening ring is analyzed. The data obtained in elastoplastic and linearly elastic formulations of the problem are compared. Cylindrical Shell (dpeaa)DE-He213 Internal Pressure (dpeaa)DE-He213 Spherical Shell (dpeaa)DE-He213 Elliptical Opening (dpeaa)DE-He213 Nonlinear Deformation (dpeaa)DE-He213 Storozhuk, E. A. verfasserin aut Chernyshenko, I. S. verfasserin aut Enthalten in International applied mechanics New York, NY [u.a.] : Consultants Bureau, 1966 35(1999), 5 vom: Mai, Seite 508-514 (DE-627)32557040X (DE-600)2037331-4 1573-8582 nnns volume:35 year:1999 number:5 month:05 pages:508-514 https://dx.doi.org/10.1007/BF03355411 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_121 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_374 GBV_ILN_602 GBV_ILN_636 GBV_ILN_647 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2018 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2043 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2158 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2193 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_2808 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4277 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4346 GBV_ILN_4367 GBV_ILN_4393 GBV_ILN_4700 GBV_ILN_4753 50.31 ASE AR 35 1999 5 05 508-514 |
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Enthalten in International applied mechanics 35(1999), 5 vom: Mai, Seite 508-514 volume:35 year:1999 number:5 month:05 pages:508-514 |
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Enthalten in International applied mechanics 35(1999), 5 vom: Mai, Seite 508-514 volume:35 year:1999 number:5 month:05 pages:508-514 |
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Cylindrical Shell Internal Pressure Spherical Shell Elliptical Opening Nonlinear Deformation |
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International applied mechanics |
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Mulyar, V. P. @@aut@@ Storozhuk, E. A. @@aut@@ Chernyshenko, I. S. @@aut@@ |
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1999-05-01T00:00:00Z |
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| author |
Mulyar, V. P. |
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Mulyar, V. P. ddc 530 bkl 50.31 misc Cylindrical Shell misc Internal Pressure misc Spherical Shell misc Elliptical Opening misc Nonlinear Deformation On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit |
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530 ASE 50.31 bkl On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit Cylindrical Shell (dpeaa)DE-He213 Internal Pressure (dpeaa)DE-He213 Spherical Shell (dpeaa)DE-He213 Elliptical Opening (dpeaa)DE-He213 Nonlinear Deformation (dpeaa)DE-He213 |
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ddc 530 bkl 50.31 misc Cylindrical Shell misc Internal Pressure misc Spherical Shell misc Elliptical Opening misc Nonlinear Deformation |
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ddc 530 bkl 50.31 misc Cylindrical Shell misc Internal Pressure misc Spherical Shell misc Elliptical Opening misc Nonlinear Deformation |
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ddc 530 bkl 50.31 misc Cylindrical Shell misc Internal Pressure misc Spherical Shell misc Elliptical Opening misc Nonlinear Deformation |
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Elektronische Aufsätze Aufsätze Elektronische Ressource |
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On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit |
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| title_full |
On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit |
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Mulyar, V. P. |
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International applied mechanics |
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International applied mechanics |
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Mulyar, V. P. Storozhuk, E. A. Chernyshenko, I. S. |
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530 ASE 50.31 bkl |
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Elektronische Aufsätze |
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Mulyar, V. P. |
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10.1007/BF03355411 |
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verfasserin |
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on the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit |
| title_auth |
On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit |
| abstract |
Abstract The basic nonlinear relations describing the stress-strain state of flexible thin-walled elements (rods, rings) that stiffen the contour of curvilinear openings in shells with allowance for the plastic deformation of their materials are presented. The Lagrange variation equation is used to obtain sets of nonlinear resolving equations for a shell with a stiffened elliptical opening. Successive-approximation and finite-element methods are used to solve the nonlinear problems. Numerical results are given for an elastoplastic cylindrical shell loaded by an internal pressure of given intensity. The distribution of maximum stresses in the area of an elliptical opening with and without a stiffening ring is analyzed. The data obtained in elastoplastic and linearly elastic formulations of the problem are compared. |
| abstractGer |
Abstract The basic nonlinear relations describing the stress-strain state of flexible thin-walled elements (rods, rings) that stiffen the contour of curvilinear openings in shells with allowance for the plastic deformation of their materials are presented. The Lagrange variation equation is used to obtain sets of nonlinear resolving equations for a shell with a stiffened elliptical opening. Successive-approximation and finite-element methods are used to solve the nonlinear problems. Numerical results are given for an elastoplastic cylindrical shell loaded by an internal pressure of given intensity. The distribution of maximum stresses in the area of an elliptical opening with and without a stiffening ring is analyzed. The data obtained in elastoplastic and linearly elastic formulations of the problem are compared. |
| abstract_unstemmed |
Abstract The basic nonlinear relations describing the stress-strain state of flexible thin-walled elements (rods, rings) that stiffen the contour of curvilinear openings in shells with allowance for the plastic deformation of their materials are presented. The Lagrange variation equation is used to obtain sets of nonlinear resolving equations for a shell with a stiffened elliptical opening. Successive-approximation and finite-element methods are used to solve the nonlinear problems. Numerical results are given for an elastoplastic cylindrical shell loaded by an internal pressure of given intensity. The distribution of maximum stresses in the area of an elliptical opening with and without a stiffening ring is analyzed. The data obtained in elastoplastic and linearly elastic formulations of the problem are compared. |
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On the stress distribution near a stiffened elliptical opening in a cylindrical shell beyond the elastic limit |
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https://dx.doi.org/10.1007/BF03355411 |
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Storozhuk, E. A. Chernyshenko, I. S. |
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Storozhuk, E. A. Chernyshenko, I. S. |
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10.1007/BF03355411 |
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2024-07-03T18:04:45.398Z |
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| score |
7.4012203 |