Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695
Abstract Braced frames are normally used as ancillary lateral load resisting systems in engineering. The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design varia...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Sedaghatnezhad, Hadi [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2021 |
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| Schlagwörter: |
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| Anmerkung: |
© The Institution of Engineers (India) 2021 |
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| Übergeordnetes Werk: |
Enthalten in: Journal of the Institution of Engineers (India) - [New Delhi] : Springer India, 2012, 103(2021), 1 vom: 05. Okt., Seite 263-270 |
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| Übergeordnetes Werk: |
volume:103 ; year:2021 ; number:1 ; day:05 ; month:10 ; pages:263-270 |
| Links: |
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| DOI / URN: |
10.1007/s40030-021-00576-3 |
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| Katalog-ID: |
SPR046485457 |
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| 520 | |a Abstract Braced frames are normally used as ancillary lateral load resisting systems in engineering. The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design variables which these braced frames need. The design of any structural system requires seismic performance factors such as of coefficient Factor (R), over-strength factor (Ω) and displacement amplification factor ($ C_{d} $), the coefficient Factor R = 8 was obtained for Chevron brace frame with TADAS damper for this study. Also, the over-strength factor was calculated Ω0 = 2. and displacement amplification factor was calculated Cd = 4.0. The logical method implemented in the Federal Emergency Management Agency (FEMA) P695 is used to determine the quantity of these variables based on the probability of structural failure and includes nonlinear static analysis and dynamic analysis. In order to achieve over-strength and period-based ductility, nonlinear static analysis is performed. An incremental dynamic analysis is then performed to assess the CMR for different models. The different effects of the ground acceleration spectrum are considered for each model in CMR values to obtain an adjusted CMR (ACMR). Calculated values of ACMRs in areas compared to the appropriate values of FEMA P695 for probabilistic evaluation of seismic performance factors of TADAS systems and the results show that the calculated ACMR values and coefficient factor for TADAS steel system is 8, also the results show that ductility and energy absorption have increased with TADAS system. | ||
| 650 | 4 | |a TADAS dampers |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a FEMA P695 |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Coefficient factor |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a IDA analysis |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Pushover analysis |7 (dpeaa)DE-He213 | |
| 700 | 1 | |a Fallah, Ahmadali |4 aut | |
| 700 | 1 | |a Yazdi, Mohamadreza Mosalman |4 aut | |
| 700 | 1 | |a Katal Mohseni, Peyman |4 aut | |
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10.1007/s40030-021-00576-3 doi (DE-627)SPR046485457 (SPR)s40030-021-00576-3-e DE-627 ger DE-627 rakwb eng Sedaghatnezhad, Hadi verfasserin aut Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Institution of Engineers (India) 2021 Abstract Braced frames are normally used as ancillary lateral load resisting systems in engineering. The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design variables which these braced frames need. The design of any structural system requires seismic performance factors such as of coefficient Factor (R), over-strength factor (Ω) and displacement amplification factor ($ C_{d} $), the coefficient Factor R = 8 was obtained for Chevron brace frame with TADAS damper for this study. Also, the over-strength factor was calculated Ω0 = 2. and displacement amplification factor was calculated Cd = 4.0. The logical method implemented in the Federal Emergency Management Agency (FEMA) P695 is used to determine the quantity of these variables based on the probability of structural failure and includes nonlinear static analysis and dynamic analysis. In order to achieve over-strength and period-based ductility, nonlinear static analysis is performed. An incremental dynamic analysis is then performed to assess the CMR for different models. The different effects of the ground acceleration spectrum are considered for each model in CMR values to obtain an adjusted CMR (ACMR). Calculated values of ACMRs in areas compared to the appropriate values of FEMA P695 for probabilistic evaluation of seismic performance factors of TADAS systems and the results show that the calculated ACMR values and coefficient factor for TADAS steel system is 8, also the results show that ductility and energy absorption have increased with TADAS system. TADAS dampers (dpeaa)DE-He213 FEMA P695 (dpeaa)DE-He213 Coefficient factor (dpeaa)DE-He213 IDA analysis (dpeaa)DE-He213 Pushover analysis (dpeaa)DE-He213 Fallah, Ahmadali aut Yazdi, Mohamadreza Mosalman aut Katal Mohseni, Peyman aut Enthalten in Journal of the Institution of Engineers (India) [New Delhi] : Springer India, 2012 103(2021), 1 vom: 05. Okt., Seite 263-270 (DE-627)722236743 (DE-600)2677555-4 2250-2157 nnns volume:103 year:2021 number:1 day:05 month:10 pages:263-270 https://dx.doi.org/10.1007/s40030-021-00576-3 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_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 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_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 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_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_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_2118 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_2188 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_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_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_4393 GBV_ILN_4700 AR 103 2021 1 05 10 263-270 |
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10.1007/s40030-021-00576-3 doi (DE-627)SPR046485457 (SPR)s40030-021-00576-3-e DE-627 ger DE-627 rakwb eng Sedaghatnezhad, Hadi verfasserin aut Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Institution of Engineers (India) 2021 Abstract Braced frames are normally used as ancillary lateral load resisting systems in engineering. The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design variables which these braced frames need. The design of any structural system requires seismic performance factors such as of coefficient Factor (R), over-strength factor (Ω) and displacement amplification factor ($ C_{d} $), the coefficient Factor R = 8 was obtained for Chevron brace frame with TADAS damper for this study. Also, the over-strength factor was calculated Ω0 = 2. and displacement amplification factor was calculated Cd = 4.0. The logical method implemented in the Federal Emergency Management Agency (FEMA) P695 is used to determine the quantity of these variables based on the probability of structural failure and includes nonlinear static analysis and dynamic analysis. In order to achieve over-strength and period-based ductility, nonlinear static analysis is performed. An incremental dynamic analysis is then performed to assess the CMR for different models. The different effects of the ground acceleration spectrum are considered for each model in CMR values to obtain an adjusted CMR (ACMR). Calculated values of ACMRs in areas compared to the appropriate values of FEMA P695 for probabilistic evaluation of seismic performance factors of TADAS systems and the results show that the calculated ACMR values and coefficient factor for TADAS steel system is 8, also the results show that ductility and energy absorption have increased with TADAS system. TADAS dampers (dpeaa)DE-He213 FEMA P695 (dpeaa)DE-He213 Coefficient factor (dpeaa)DE-He213 IDA analysis (dpeaa)DE-He213 Pushover analysis (dpeaa)DE-He213 Fallah, Ahmadali aut Yazdi, Mohamadreza Mosalman aut Katal Mohseni, Peyman aut Enthalten in Journal of the Institution of Engineers (India) [New Delhi] : Springer India, 2012 103(2021), 1 vom: 05. Okt., Seite 263-270 (DE-627)722236743 (DE-600)2677555-4 2250-2157 nnns volume:103 year:2021 number:1 day:05 month:10 pages:263-270 https://dx.doi.org/10.1007/s40030-021-00576-3 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_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 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_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 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_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_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_2118 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_2188 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_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_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_4393 GBV_ILN_4700 AR 103 2021 1 05 10 263-270 |
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10.1007/s40030-021-00576-3 doi (DE-627)SPR046485457 (SPR)s40030-021-00576-3-e DE-627 ger DE-627 rakwb eng Sedaghatnezhad, Hadi verfasserin aut Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Institution of Engineers (India) 2021 Abstract Braced frames are normally used as ancillary lateral load resisting systems in engineering. The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design variables which these braced frames need. The design of any structural system requires seismic performance factors such as of coefficient Factor (R), over-strength factor (Ω) and displacement amplification factor ($ C_{d} $), the coefficient Factor R = 8 was obtained for Chevron brace frame with TADAS damper for this study. Also, the over-strength factor was calculated Ω0 = 2. and displacement amplification factor was calculated Cd = 4.0. The logical method implemented in the Federal Emergency Management Agency (FEMA) P695 is used to determine the quantity of these variables based on the probability of structural failure and includes nonlinear static analysis and dynamic analysis. In order to achieve over-strength and period-based ductility, nonlinear static analysis is performed. An incremental dynamic analysis is then performed to assess the CMR for different models. The different effects of the ground acceleration spectrum are considered for each model in CMR values to obtain an adjusted CMR (ACMR). Calculated values of ACMRs in areas compared to the appropriate values of FEMA P695 for probabilistic evaluation of seismic performance factors of TADAS systems and the results show that the calculated ACMR values and coefficient factor for TADAS steel system is 8, also the results show that ductility and energy absorption have increased with TADAS system. TADAS dampers (dpeaa)DE-He213 FEMA P695 (dpeaa)DE-He213 Coefficient factor (dpeaa)DE-He213 IDA analysis (dpeaa)DE-He213 Pushover analysis (dpeaa)DE-He213 Fallah, Ahmadali aut Yazdi, Mohamadreza Mosalman aut Katal Mohseni, Peyman aut Enthalten in Journal of the Institution of Engineers (India) [New Delhi] : Springer India, 2012 103(2021), 1 vom: 05. Okt., Seite 263-270 (DE-627)722236743 (DE-600)2677555-4 2250-2157 nnns volume:103 year:2021 number:1 day:05 month:10 pages:263-270 https://dx.doi.org/10.1007/s40030-021-00576-3 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_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 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_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 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_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_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_2118 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_2188 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_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_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_4393 GBV_ILN_4700 AR 103 2021 1 05 10 263-270 |
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10.1007/s40030-021-00576-3 doi (DE-627)SPR046485457 (SPR)s40030-021-00576-3-e DE-627 ger DE-627 rakwb eng Sedaghatnezhad, Hadi verfasserin aut Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Institution of Engineers (India) 2021 Abstract Braced frames are normally used as ancillary lateral load resisting systems in engineering. The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design variables which these braced frames need. The design of any structural system requires seismic performance factors such as of coefficient Factor (R), over-strength factor (Ω) and displacement amplification factor ($ C_{d} $), the coefficient Factor R = 8 was obtained for Chevron brace frame with TADAS damper for this study. Also, the over-strength factor was calculated Ω0 = 2. and displacement amplification factor was calculated Cd = 4.0. The logical method implemented in the Federal Emergency Management Agency (FEMA) P695 is used to determine the quantity of these variables based on the probability of structural failure and includes nonlinear static analysis and dynamic analysis. In order to achieve over-strength and period-based ductility, nonlinear static analysis is performed. An incremental dynamic analysis is then performed to assess the CMR for different models. The different effects of the ground acceleration spectrum are considered for each model in CMR values to obtain an adjusted CMR (ACMR). Calculated values of ACMRs in areas compared to the appropriate values of FEMA P695 for probabilistic evaluation of seismic performance factors of TADAS systems and the results show that the calculated ACMR values and coefficient factor for TADAS steel system is 8, also the results show that ductility and energy absorption have increased with TADAS system. TADAS dampers (dpeaa)DE-He213 FEMA P695 (dpeaa)DE-He213 Coefficient factor (dpeaa)DE-He213 IDA analysis (dpeaa)DE-He213 Pushover analysis (dpeaa)DE-He213 Fallah, Ahmadali aut Yazdi, Mohamadreza Mosalman aut Katal Mohseni, Peyman aut Enthalten in Journal of the Institution of Engineers (India) [New Delhi] : Springer India, 2012 103(2021), 1 vom: 05. Okt., Seite 263-270 (DE-627)722236743 (DE-600)2677555-4 2250-2157 nnns volume:103 year:2021 number:1 day:05 month:10 pages:263-270 https://dx.doi.org/10.1007/s40030-021-00576-3 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_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 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_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 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_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_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_2118 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_2188 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_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_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_4393 GBV_ILN_4700 AR 103 2021 1 05 10 263-270 |
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10.1007/s40030-021-00576-3 doi (DE-627)SPR046485457 (SPR)s40030-021-00576-3-e DE-627 ger DE-627 rakwb eng Sedaghatnezhad, Hadi verfasserin aut Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Institution of Engineers (India) 2021 Abstract Braced frames are normally used as ancillary lateral load resisting systems in engineering. The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design variables which these braced frames need. The design of any structural system requires seismic performance factors such as of coefficient Factor (R), over-strength factor (Ω) and displacement amplification factor ($ C_{d} $), the coefficient Factor R = 8 was obtained for Chevron brace frame with TADAS damper for this study. Also, the over-strength factor was calculated Ω0 = 2. and displacement amplification factor was calculated Cd = 4.0. The logical method implemented in the Federal Emergency Management Agency (FEMA) P695 is used to determine the quantity of these variables based on the probability of structural failure and includes nonlinear static analysis and dynamic analysis. In order to achieve over-strength and period-based ductility, nonlinear static analysis is performed. An incremental dynamic analysis is then performed to assess the CMR for different models. The different effects of the ground acceleration spectrum are considered for each model in CMR values to obtain an adjusted CMR (ACMR). Calculated values of ACMRs in areas compared to the appropriate values of FEMA P695 for probabilistic evaluation of seismic performance factors of TADAS systems and the results show that the calculated ACMR values and coefficient factor for TADAS steel system is 8, also the results show that ductility and energy absorption have increased with TADAS system. TADAS dampers (dpeaa)DE-He213 FEMA P695 (dpeaa)DE-He213 Coefficient factor (dpeaa)DE-He213 IDA analysis (dpeaa)DE-He213 Pushover analysis (dpeaa)DE-He213 Fallah, Ahmadali aut Yazdi, Mohamadreza Mosalman aut Katal Mohseni, Peyman aut Enthalten in Journal of the Institution of Engineers (India) [New Delhi] : Springer India, 2012 103(2021), 1 vom: 05. Okt., Seite 263-270 (DE-627)722236743 (DE-600)2677555-4 2250-2157 nnns volume:103 year:2021 number:1 day:05 month:10 pages:263-270 https://dx.doi.org/10.1007/s40030-021-00576-3 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_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 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_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 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_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_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_2118 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_2188 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_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_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_4393 GBV_ILN_4700 AR 103 2021 1 05 10 263-270 |
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The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design variables which these braced frames need. The design of any structural system requires seismic performance factors such as of coefficient Factor (R), over-strength factor (Ω) and displacement amplification factor ($ C_{d} $), the coefficient Factor R = 8 was obtained for Chevron brace frame with TADAS damper for this study. Also, the over-strength factor was calculated Ω0 = 2. and displacement amplification factor was calculated Cd = 4.0. The logical method implemented in the Federal Emergency Management Agency (FEMA) P695 is used to determine the quantity of these variables based on the probability of structural failure and includes nonlinear static analysis and dynamic analysis. In order to achieve over-strength and period-based ductility, nonlinear static analysis is performed. An incremental dynamic analysis is then performed to assess the CMR for different models. The different effects of the ground acceleration spectrum are considered for each model in CMR values to obtain an adjusted CMR (ACMR). Calculated values of ACMRs in areas compared to the appropriate values of FEMA P695 for probabilistic evaluation of seismic performance factors of TADAS systems and the results show that the calculated ACMR values and coefficient factor for TADAS steel system is 8, also the results show that ductility and energy absorption have increased with TADAS system.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">TADAS dampers</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">FEMA P695</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Coefficient factor</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">IDA analysis</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Pushover analysis</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Fallah, Ahmadali</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Yazdi, Mohamadreza Mosalman</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Katal Mohseni, Peyman</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Journal of the Institution of Engineers (India)</subfield><subfield code="d">[New Delhi] : Springer India, 2012</subfield><subfield code="g">103(2021), 1 vom: 05. 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| author |
Sedaghatnezhad, Hadi |
| spellingShingle |
Sedaghatnezhad, Hadi misc TADAS dampers misc FEMA P695 misc Coefficient factor misc IDA analysis misc Pushover analysis Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 |
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| topic_title |
Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 TADAS dampers (dpeaa)DE-He213 FEMA P695 (dpeaa)DE-He213 Coefficient factor (dpeaa)DE-He213 IDA analysis (dpeaa)DE-He213 Pushover analysis (dpeaa)DE-He213 |
| topic |
misc TADAS dampers misc FEMA P695 misc Coefficient factor misc IDA analysis misc Pushover analysis |
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misc TADAS dampers misc FEMA P695 misc Coefficient factor misc IDA analysis misc Pushover analysis |
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Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 |
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Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 |
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Sedaghatnezhad, Hadi |
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Journal of the Institution of Engineers (India) |
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Sedaghatnezhad, Hadi Fallah, Ahmadali Yazdi, Mohamadreza Mosalman Katal Mohseni, Peyman |
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Elektronische Aufsätze |
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Sedaghatnezhad, Hadi |
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10.1007/s40030-021-00576-3 |
| title_sort |
investigation of seismic coefficient factor for divergent bracing frame with tadas damper utilizing the fema p695 |
| title_auth |
Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 |
| abstract |
Abstract Braced frames are normally used as ancillary lateral load resisting systems in engineering. The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design variables which these braced frames need. The design of any structural system requires seismic performance factors such as of coefficient Factor (R), over-strength factor (Ω) and displacement amplification factor ($ C_{d} $), the coefficient Factor R = 8 was obtained for Chevron brace frame with TADAS damper for this study. Also, the over-strength factor was calculated Ω0 = 2. and displacement amplification factor was calculated Cd = 4.0. The logical method implemented in the Federal Emergency Management Agency (FEMA) P695 is used to determine the quantity of these variables based on the probability of structural failure and includes nonlinear static analysis and dynamic analysis. In order to achieve over-strength and period-based ductility, nonlinear static analysis is performed. An incremental dynamic analysis is then performed to assess the CMR for different models. The different effects of the ground acceleration spectrum are considered for each model in CMR values to obtain an adjusted CMR (ACMR). Calculated values of ACMRs in areas compared to the appropriate values of FEMA P695 for probabilistic evaluation of seismic performance factors of TADAS systems and the results show that the calculated ACMR values and coefficient factor for TADAS steel system is 8, also the results show that ductility and energy absorption have increased with TADAS system. © The Institution of Engineers (India) 2021 |
| abstractGer |
Abstract Braced frames are normally used as ancillary lateral load resisting systems in engineering. The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design variables which these braced frames need. The design of any structural system requires seismic performance factors such as of coefficient Factor (R), over-strength factor (Ω) and displacement amplification factor ($ C_{d} $), the coefficient Factor R = 8 was obtained for Chevron brace frame with TADAS damper for this study. Also, the over-strength factor was calculated Ω0 = 2. and displacement amplification factor was calculated Cd = 4.0. The logical method implemented in the Federal Emergency Management Agency (FEMA) P695 is used to determine the quantity of these variables based on the probability of structural failure and includes nonlinear static analysis and dynamic analysis. In order to achieve over-strength and period-based ductility, nonlinear static analysis is performed. An incremental dynamic analysis is then performed to assess the CMR for different models. The different effects of the ground acceleration spectrum are considered for each model in CMR values to obtain an adjusted CMR (ACMR). Calculated values of ACMRs in areas compared to the appropriate values of FEMA P695 for probabilistic evaluation of seismic performance factors of TADAS systems and the results show that the calculated ACMR values and coefficient factor for TADAS steel system is 8, also the results show that ductility and energy absorption have increased with TADAS system. © The Institution of Engineers (India) 2021 |
| abstract_unstemmed |
Abstract Braced frames are normally used as ancillary lateral load resisting systems in engineering. The TADAS damper (Triangular Added Damping and Stiffness) has an important effect on energy absorption. Design of TADAS frame structures is based on common design rules and evaluation of design variables which these braced frames need. The design of any structural system requires seismic performance factors such as of coefficient Factor (R), over-strength factor (Ω) and displacement amplification factor ($ C_{d} $), the coefficient Factor R = 8 was obtained for Chevron brace frame with TADAS damper for this study. Also, the over-strength factor was calculated Ω0 = 2. and displacement amplification factor was calculated Cd = 4.0. The logical method implemented in the Federal Emergency Management Agency (FEMA) P695 is used to determine the quantity of these variables based on the probability of structural failure and includes nonlinear static analysis and dynamic analysis. In order to achieve over-strength and period-based ductility, nonlinear static analysis is performed. An incremental dynamic analysis is then performed to assess the CMR for different models. The different effects of the ground acceleration spectrum are considered for each model in CMR values to obtain an adjusted CMR (ACMR). Calculated values of ACMRs in areas compared to the appropriate values of FEMA P695 for probabilistic evaluation of seismic performance factors of TADAS systems and the results show that the calculated ACMR values and coefficient factor for TADAS steel system is 8, also the results show that ductility and energy absorption have increased with TADAS system. © The Institution of Engineers (India) 2021 |
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| title_short |
Investigation of Seismic Coefficient Factor for Divergent Bracing Frame with TADAS Damper Utilizing the FEMA P695 |
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https://dx.doi.org/10.1007/s40030-021-00576-3 |
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| author2 |
Fallah, Ahmadali Yazdi, Mohamadreza Mosalman Katal Mohseni, Peyman |
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Fallah, Ahmadali Yazdi, Mohamadreza Mosalman Katal Mohseni, Peyman |
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| doi_str |
10.1007/s40030-021-00576-3 |
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2024-07-03T22:49:40.250Z |
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| score |
7.3996468 |