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Proc. ASME. GT2010, Volume 5: Industrial and Cogeneration; Microturbines and Small Turbomachinery; Oil and Gas Applications; Wind Turbine Technology, 109-120, June 14–18, 2010

Paper No: GT2010-22959

DOI: https://doi.org/10.1115/GT2010-22959

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Topics: Design, Pressure, Organic Rankine cycle, Temperature, Fluids, Nozzles, Cycles, Flow (Dynamics), Probes, Siloxanes

Journal Articles

A Parametric Study of the Blade Row Interaction in a High Pressure Turbine Stage

G. Persico, P. Gaetani, C. Osnaghi

J. Turbomach. July 2009, 131(3): 031006.

DOI: https://doi.org/10.1115/1.2987236

Published Online: April 8, 2009

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Topics: Flow (Dynamics), Rotors, Stators, Blades, Vortices, Wakes

Proceedings Papers

Effects of Off-Design Operating Conditions on the Blade Row Interaction in a HP Turbine Stage

G. Persico, P. Gaetani, C. Osnaghi

Proc. ASME. GT2007, Volume 6: Turbo Expo 2007, Parts A and B, 503-517, May 14–17, 2007

Paper No: GT2007-27185

DOI: https://doi.org/10.1115/GT2007-27185

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Topics: Blades, Design, Turbines, Rotors, Stators, Flow (Dynamics), Vortices, Probes, Cascades (Fluid dynamics), Chords (Trusses)

Proceedings Papers

Investigation of the Flow Field in a HP Turbine Stage for Two Stator-Rotor Axial Gaps: Part I — 3D Time-Averaged Flow Field

P. Gaetani, G. Persico, V. Dossena, C. Osnaghi

Proc. ASME. GT2006, Volume 6: Turbomachinery, Parts A and B, 659-668, May 8–11, 2006

Paper No: GT2006-90553

DOI: https://doi.org/10.1115/GT2006-90553

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Topics: Flow (Dynamics), Rotors, Stators, Turbines, Blades, Probes, Experimental analysis, Gas turbines, High pressure (Physics), Temperature sensors

Proceedings Papers

Investigation of the Flow Field in a HP Turbine Stage for Two Stator-Rotor Axial Gaps: Part II — Unsteady Flow Field

P. Gaetani, G. Persico, V. Dossena, C. Osnaghi

Proc. ASME. GT2006, Volume 6: Turbomachinery, Parts A and B, 669-680, May 8–11, 2006

Paper No: GT2006-90556

DOI: https://doi.org/10.1115/GT2006-90556

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Topics: Flow (Dynamics), Rotors, Stators, Turbines, Unsteady flow, Vortices, Cascades (Fluid dynamics), Chords (Trusses), Probes, Wakes

Proceedings Papers

Erratum: “On the Influence of Back Pressure and Size on the Performance of Safety Valves” [ASME 2002 Pressure Vessels and Piping Conference, Piping and Component Analysis and Diagnosis, Vancouver, BC, Canada, August 5–9, 2002, Conference Sponsors: Pressure Vessels and Piping Division, ISBN: 0-7918-4658-X, Copyright © 2002 by ASME. Paper No. PVP2002-1514, pp. 35-41; 7 pages; doi:10.1115/PVP2002-1514]

V. Dossena, P. Gaetani, F. Marinoni, C. Osnaghi

Proc. ASME. PVP2002, Piping and Component Analysis and Diagnosis, 147-148, August 5–9, 2002

Paper No: PVP2002-1514e

DOI: https://doi.org/10.1115/PVP2002-1514e

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Topics: Pipes, Pressure, Pressure vessels, Safety, Valves, Errors

Proceedings Papers

On the Influence of Back Pressure and Size on the Performance of Safety Valves

V. Dossena, P. Gaetani, F. Marinoni, C. Osnaghi

Proc. ASME. PVP2002, Piping and Component Analysis and Diagnosis, 35-41, August 5–9, 2002

Paper No: PVP2002-1514

DOI: https://doi.org/10.1115/PVP2002-1514

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Topics: Pressure, Safety, Valves, Flow (Dynamics), American Petroleum Institute, Dimensions, Disks, Design, Discharge coefficient, Sensitivity analysis

Journal Articles

Investigation of the Flow Field in a High-Pressure Turbine Stage for Two Stator-Rotor Axial Gaps—Part I: Three-Dimensional Time-Averaged Flow Field

P. Gaetani, G. Persico, V. Dossena, C. Osnaghi

J. Turbomach. July 2007, 129(3): 572–579.

DOI: https://doi.org/10.1115/1.2472383

Published Online: July 28, 2006

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Topics: Blades, Flow (Dynamics), Rotors, Stators, Turbines

Journal Articles

Investigation of the Flow Field in a High-Pressure Turbine Stage for Two Stator-Rotor Axial Gaps—Part II: Unsteady Flow Field

P. Gaetani, G. Persico, V. Dossena, C. Osnaghi

J. Turbomach. July 2007, 129(3): 580–590.

DOI: https://doi.org/10.1115/1.2472393

Published Online: July 23, 2006

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Topics: Flow (Dynamics), Rotors, Stators, Wakes, Vortices

Journal Articles

Secondary Flows in a Transonic Cascade: Comparison Between Experimental and Numerical Results

F. Bassi, C. Osnaghi, A. Perdichizzi, M. Savini

J. Fluids Eng. December 1989, 111(4): 369–377.

DOI: https://doi.org/10.1115/1.3243655

Published Online: December 1, 1989

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Topics: Cascades (Fluid dynamics), Flow (Dynamics), Vortices, Blades, Boundary layers, Boundary-value problems, Compressibility, Computation, Finite volume methods, Mach number

Journal citation

NARROW

The Influence of Film-Cooling on the Aerodynamic Performance of a Turbine Nozzle Guide Vane

Impeller-Vaned Diffuser Interaction in a Centrifugal Compressor at Off Design Conditions

Impeller–Vaned Diffuser Interaction in a Centrifugal Compressor at the Best Efficiency Point

Impeller–Vaned Diffuser Interaction in a Centrifugal Compressor at Off Design Conditions

Design of a Test Rig for Organic Vapours

A Parametric Study of the Blade Row Interaction in a High Pressure Turbine Stage

Effects of Off-Design Operating Conditions on the Blade Row Interaction in a HP Turbine Stage

Investigation of the Flow Field in a HP Turbine Stage for Two Stator-Rotor Axial Gaps: Part I — 3D Time-Averaged Flow Field

Investigation of the Flow Field in a HP Turbine Stage for Two Stator-Rotor Axial Gaps: Part II — Unsteady Flow Field

On the Influence of Back Pressure and Size on the Performance of Safety Valves

Investigation of the Flow Field in a High-Pressure Turbine Stage for Two Stator-Rotor Axial Gaps—Part I: Three-Dimensional Time-Averaged Flow Field

Investigation of the Flow Field in a High-Pressure Turbine Stage for Two Stator-Rotor Axial Gaps—Part II: Unsteady Flow Field

Secondary Flows in a Transonic Cascade: Comparison Between Experimental and Numerical Results

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