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Date of download: 10/19/2017 Copyright © ASME. All rights reserved. From: Influence of Molecular Complexity on Nozzle Design for an Organic Vapor Wind Tunnel J. Eng. Gas Turbines Power. 2013;135(4):042307-042307-6. doi:10.1115/1.4023117 Figure Legend: Reference nozzle expansion process in the T-s plane for siloxane fluid MDM. Left: case initial and final state point 6 and 7. Right: expansion states superimposed to the iso-Γ lines.

Date of download: 10/19/2017 Copyright © ASME. All rights reserved. From: Influence of Molecular Complexity on Nozzle Design for an Organic Vapor Wind Tunnel J. Eng. Gas Turbines Power. 2013;135(4):042307-042307-6. doi:10.1115/1.4023117 Figure Legend: Sketch of the TROVA test rig. State points are also indicated.

Date of download: 10/19/2017 Copyright © ASME. All rights reserved. From: Influence of Molecular Complexity on Nozzle Design for an Organic Vapor Wind Tunnel J. Eng. Gas Turbines Power. 2013;135(4):042307-042307-6. doi:10.1115/1.4023117 Figure Legend: Mach number (a), pressure (b), temperature (c), and fundamental derivative (d) fields for the design case in Table 1, using both the real gas (SW, top) and ideal gas (PIG, bottom) models

Date of download: 10/19/2017 Copyright © ASME. All rights reserved. From: Influence of Molecular Complexity on Nozzle Design for an Organic Vapor Wind Tunnel J. Eng. Gas Turbines Power. 2013;135(4):042307-042307-6. doi:10.1115/1.4023117 Figure Legend: Mach number (a), pressure (b), temperature number (c), and Γ (d) profiles for design case in Table 1, using the real and the ideal gas models. The solid lines refer to the nozzle wall and the dash-dotted lines refer to the nozzle axis of symmetry.

Date of download: 10/19/2017 Copyright © ASME. All rights reserved. From: Influence of Molecular Complexity on Nozzle Design for an Organic Vapor Wind Tunnel J. Eng. Gas Turbines Power. 2013;135(4):042307-042307-6. doi:10.1115/1.4023117 Figure Legend: Nozzle geometry for fluids of different molecular complexity for TT,6/Tc=0.975, PT,6/Pc=0.78, and β=PT,6/P7=25. Left: geometry of the divergent section. Right: detail of the exit section.