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A Robust Adiabatic Model for a Quasi-Steady Prediction of Far-Off Non-Measured Performance in Vaneless Twin-Entry or Dual-Volute Radial Turbines

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A Robust Adiabatic Model for a Quasi-Steady Prediction of Far-Off Non-Measured Performance in Vaneless Twin-Entry or Dual-Volute Radial Turbines

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Serrano, J.; Arnau Martínez, FJ.; García-Cuevas González, LM.; Samala, V. (2020). A Robust Adiabatic Model for a Quasi-Steady Prediction of Far-Off Non-Measured Performance in Vaneless Twin-Entry or Dual-Volute Radial Turbines. Applied Sciences. 10(6):1-43. https://doi.org/10.3390/app10061955

Por favor, use este identificador para citar o enlazar este ítem: http://hdl.handle.net/10251/166581

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Título: A Robust Adiabatic Model for a Quasi-Steady Prediction of Far-Off Non-Measured Performance in Vaneless Twin-Entry or Dual-Volute Radial Turbines
Autor: Serrano, J.R. Arnau Martínez, Francisco José García-Cuevas González, Luis Miguel Samala, Vishnu
Entidad UPV: Universitat Politècnica de València. Departamento de Máquinas y Motores Térmicos - Departament de Màquines i Motors Tèrmics
Fecha difusión:
Resumen:
[EN] The current investigation describes in detail a mass flow oriented model for extrapolation of reduced mass flow and adiabatic efficiency of double entry radial inflow turbines under any unequal and partial flow admission ...[+]
Palabras clave: Turbocharger , Twin-entry radial turbines , Dual-volute radial turbines , Unequal and partial flow admission , Quasi-steady models , Adiabatic efficiency model , Reduced mass flow model
Derechos de uso: Reconocimiento (by)
Fuente:
Applied Sciences. (eissn: 2076-3417 )
DOI: 10.3390/app10061955
Editorial:
MDPI AG
Versión del editor: https://doi.org/10.3390/app10061955
Código del Proyecto:
info:eu-repo/grantAgreement/UPV//PAID-06-18/
info:eu-repo/grantAgreement/UPV//FPI-2017-S2-1256/
Agradecimientos:
Vishnu Samala is partially supported through contract FPI-2017-S2-1256 of Programa de Apoyo para la Investigacion y Desarrollo (PAID) of Universitat Politecnica de Valencia. This work was partially funded by the 'Ayuda a ...[+]
Tipo: Artículo

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