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Date of download: 11/11/2017 Copyright © ASME. All rights reserved.

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1 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Three-Dimensional sketch of the piping system

2 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Two-dimensional sketch of the piping system: (a) layout #1 and (b) layout #2

3 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Diagram of the control and acquisition system

4 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Steady-state performance map: pressure ratio

5 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Steady-state performance maps: isentropic efficiency

6 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Steady-state performance maps: static pressure ratio at stage five (bleed valve position)

7 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Dynamic test at ν = 10,000 rpm

8 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Dynamic test at ν = 10,000 rpm. Typical surge oscillations encountered on p2, m1, m3, and Pmec,norm.

9 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Dynamic test at ν = 10,000 rpm. Characteristic curve toward surge and recover from surge.

10 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Dynamic test at ν = 15,000 rpm. Surge pulsations of p2, m1, m3, and Pmec,norm.

11 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Dynamic test at ν = 10,000 rpm. Fast-response transducers signals at compressor a few instants before surge.

12 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Dynamic test at ν = 10,000 rpm. Stall analysis at compressor inlet. Frequency domain analysis.

13 Date of download: 11/11/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation of Stall and Surge in a Multistage Compressor J. Eng. Gas Turbines Power. 2016;139(2): doi: / Figure Legend: Dynamic test at ν = 10,000 rpm. Stall analysis at compressor inlet. Complete development of rotating perturbations.


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