Bibliographic citations
Albinacorta, E., Ramirez, R. (2023). Calibración por retroanálisis de los parámetros geotécnicos considerando la prueba de Celda de Osterberg en pilotes mediante la técnica de elementos finitos [Trabajo de Suficiencia Profesional, Universidad Peruana de Ciencias Aplicadas (UPC)]. http://hdl.handle.net/10757/670391
Albinacorta, E., Ramirez, R. Calibración por retroanálisis de los parámetros geotécnicos considerando la prueba de Celda de Osterberg en pilotes mediante la técnica de elementos finitos [Trabajo de Suficiencia Profesional]. PE: Universidad Peruana de Ciencias Aplicadas (UPC); 2023. http://hdl.handle.net/10757/670391
@misc{renati/410147,
title = "Calibración por retroanálisis de los parámetros geotécnicos considerando la prueba de Celda de Osterberg en pilotes mediante la técnica de elementos finitos",
author = "Ramirez Guisse, Rodrigo Marcel",
publisher = "Universidad Peruana de Ciencias Aplicadas (UPC)",
year = "2023"
}
With the objective of overcoming the limitations given by the Osterberg Cell in terms of the amount of load applied to the pilots and the capacity of the pilots, a finite element analysis was carried out using the O-Cell tests carried out on Linea 2 del metro de Lima. The San Juan de Dios station was chosen as the test to be used and an analysis of the testing procedure was carried out as well as the increases and decreases in load and the geotechnical tests made in the field. Taking this information into account, the test was modeled in Plaxis 2D, finding inconsistencies in the results obtained in the Insitu test. Firstly, it was found that the soil fails under the application of a load of 23.1 MN, as well as displacements 6 times larger than the ones measure Insitu. Given this, the inputs with the greatest influence were identified, these being the cohesion and friction angle of the soil, and an analysis of direct cutting tests carried out on typical gravel from the Lima conglomerate was carried out. New geotechnical properties were defined, and modeling was performed again. This new calibrated model had a 90% approximation of downward displacements and a 60% approximation of upward displacements. Likewise, soil failure is avoided, which allows displacements to be found for higher load applications. It was identified that the differences found were due to a difference in the methodology of the Plaxis 2D Software, these differences are the load application time, the need to increase the number of strata and the creep effect that occurs in the pilot and ground.
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