Biblio

Found 27 results
Author [ Keyword(Desc)] Type Year
Filters: Author is Alberto Scotti Del Greco  [Clear All Filters]
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Adiabatic wall temperature
Innocenti G, Marconcini M, Michelassi V, Ciani A, Jurek T, Scotti Del Greco A, Pacciani R.  2025.  On the Assessment of CFD Assumptions for the Preliminary Design of a Two-Stage High-Pressure Turbine: Impact of Unsteady Effects on Thermal Loads. Int. J. Heat Mass Transf. 236(1)
Aeromechanics
Innocenti G, Miris L, Pinelli L, Del Vescovo G, Beghini E, Tripoli G, Scotti Del Greco A, Marconcini M.  2025.  Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T36A022.
GT2025-153843
axial compressor
Burberi C, Michelassi V, Scotti Del Greco A, Lorusso S, Tapinassi L, Marconcini M, Pacciani R.  2020.  Validation of Steady and Unsteady CFD Strategies in the Design of Axial Compressors for Gas Turbine Engines. Aerospace Science and Technology. 107:106307.
CFD
Burberi C, Michelassi V, Scotti Del Greco A, Lorusso S, Tapinassi L, Marconcini M, Pacciani R.  2020.  Validation of Steady and Unsteady CFD Strategies in the Design of Axial Compressors for Gas Turbine Engines. Aerospace Science and Technology. 107:106307.
Clocking
Arnone A, Marconcini M, Scotti Del Greco A, Spano E.  2004.  Numerical Investigation of Three-Dimensional Clocking Effects in a Low Pressure Turbine. ASME Journal of Turbomachinery. 126(3):375–384.
Design
Burberi C, Michelassi V, Scotti Del Greco A, Lorusso S, Tapinassi L, Marconcini M, Pacciani R.  2020.  Validation of Steady and Unsteady CFD Strategies in the Design of Axial Compressors for Gas Turbine Engines. Aerospace Science and Technology. 107:106307.
Heat Transfer
Facchini B, Magi A, Scotti Del Greco A.  2004.  Conjugate Heat Transfer Simulation of a Radially Cooled Gas Turbine Vane. ASME Turbo Expo 2004: Power for Land, Sea, and Air. 3:951-961.
June 14–17, Vienna, Austria, ASME paper GT2004-54213
High Lift
Arnone A, Bonaiuti D, Focacci A, Pacciani R, Scotti Del Greco A, Spano E.  2004.  Parametric Optimization of a High-Lift Turbine Vane. Conf. Proc. Vol. 5: Turbo Expo 2004, Parts A and B. :1469–1479.
June 14–17, Vienna, Austria, ASME paper GT2004-54308
HPT
Innocenti G, Marconcini M, Michelassi V, Ciani A, Jurek T, Scotti Del Greco A, Pacciani R.  2025.  On the Assessment of CFD Assumptions for the Preliminary Design of a Two-Stage High-Pressure Turbine: Impact of Unsteady Effects on Thermal Loads. Int. J. Heat Mass Transf. 236(1)
low engine order
Innocenti G, Miris L, Pinelli L, Del Vescovo G, Beghini E, Tripoli G, Scotti Del Greco A, Marconcini M.  2025.  Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T36A022.
GT2025-153843
LPT
Arnone A, Bonaiuti D, Focacci A, Pacciani R, Scotti Del Greco A, Spano E.  2004.  Parametric Optimization of a High-Lift Turbine Vane. Conf. Proc. Vol. 5: Turbo Expo 2004, Parts A and B. :1469–1479.
June 14–17, Vienna, Austria, ASME paper GT2004-54308
optical probe
Innocenti G, Miris L, Pinelli L, Del Vescovo G, Beghini E, Tripoli G, Scotti Del Greco A, Marconcini M.  2025.  Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T36A022.
GT2025-153843
Optimization
Arnone A, Bonaiuti D, Focacci A, Pacciani R, Scotti Del Greco A, Spano E.  2004.  Parametric Optimization of a High-Lift Turbine Vane. Conf. Proc. Vol. 5: Turbo Expo 2004, Parts A and B. :1469–1479.
June 14–17, Vienna, Austria, ASME paper GT2004-54308
ORC
Marconcini M, Rubechini F, Arnone A, Scotti Del Greco A, Biagi R.  2012.  Aerodynamic Investigation of a High Pressure Ratio Turbo-Expander for Organic Rankine Cycle Applications. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. 8: Turbomachinery, Parts A, B, and C:847-856.
ASME paper GT2012-69409.
Rubechini F, Marconcini M, Arnone A, Scotti Del Greco A, Biagi R.  2013.  Special Challenges in the Computational Fluid Dynamics Modeling of Transonic Turbo-Expanders. ASME Journal of Engineering for Gas Turbines and Power. 135:102701.
ASME paper GT2013-95554
performance
Arnone A, Marconcini M, Scotti Del Greco A, Spano E.  2004.  Numerical Investigation of Three-Dimensional Clocking Effects in a Low Pressure Turbine. ASME Journal of Turbomachinery. 126(3):375–384.
preliminary design
Innocenti G, Marconcini M, Michelassi V, Ciani A, Jurek T, Scotti Del Greco A, Pacciani R.  2025.  On the Assessment of CFD Assumptions for the Preliminary Design of a Two-Stage High-Pressure Turbine: Impact of Unsteady Effects on Thermal Loads. Int. J. Heat Mass Transf. 236(1)
Real Gas
Marconcini M, Rubechini F, Arnone A, Scotti Del Greco A, Biagi R.  2012.  Aerodynamic Investigation of a High Pressure Ratio Turbo-Expander for Organic Rankine Cycle Applications. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. 8: Turbomachinery, Parts A, B, and C:847-856.
ASME paper GT2012-69409.
Rubechini F, Marconcini M, Arnone A, Scotti Del Greco A, Biagi R.  2013.  Special Challenges in the Computational Fluid Dynamics Modeling of Transonic Turbo-Expanders. ASME Journal of Engineering for Gas Turbines and Power. 135:102701.
ASME paper GT2013-95554
Turbo-Expander
Marconcini M, Rubechini F, Arnone A, Scotti Del Greco A, Biagi R.  2012.  Aerodynamic Investigation of a High Pressure Ratio Turbo-Expander for Organic Rankine Cycle Applications. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. 8: Turbomachinery, Parts A, B, and C:847-856.
ASME paper GT2012-69409.
Rubechini F, Marconcini M, Arnone A, Scotti Del Greco A, Biagi R.  2013.  Special Challenges in the Computational Fluid Dynamics Modeling of Transonic Turbo-Expanders. ASME Journal of Engineering for Gas Turbines and Power. 135:102701.
ASME paper GT2013-95554
unsteady CFD
Innocenti G, Miris L, Pinelli L, Del Vescovo G, Beghini E, Tripoli G, Scotti Del Greco A, Marconcini M.  2025.  Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T36A022.
GT2025-153843
Unsteady Flows
Arnone A, Marconcini M, Scotti Del Greco A, Spano E.  2004.  Numerical Investigation of Three-Dimensional Clocking Effects in a Low Pressure Turbine. ASME Journal of Turbomachinery. 126(3):375–384.
Rubechini F, Marconcini M, Arnone A, Scotti Del Greco A, Biagi R.  2013.  Special Challenges in the Computational Fluid Dynamics Modeling of Transonic Turbo-Expanders. ASME Journal of Engineering for Gas Turbines and Power. 135:102701.
ASME paper GT2013-95554
URANS
Innocenti G, Marconcini M, Michelassi V, Ciani A, Jurek T, Scotti Del Greco A, Pacciani R.  2025.  On the Assessment of CFD Assumptions for the Preliminary Design of a Two-Stage High-Pressure Turbine: Impact of Unsteady Effects on Thermal Loads. Int. J. Heat Mass Transf. 236(1)

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