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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: Effects of ambient pressure, temperature, and RH changes on the enthalpy, density, and ratio of specific heats of air
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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: Compressor flowpath including station numbering scheme
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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: Difference in TPR between a hot and cold day at 3% and 4% TC
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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: Percent difference change in TPR with density and work coefficient correction on a hot and cold day
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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: Reynolds number index on a hot and cold day
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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: Reynolds number fluctuations with ambient inlet conditions: (a) temperature, (b) RH, and (c) pressure
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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: TPR variations with ambient temperature for three nominal TCs: (a) 1.5% TC, (b) 3% TC, and (c) 4% TC
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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: Total pressure wakes at 80% span for 3% TC at near-stall loading conditions, hot and cold days
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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: Radial total pressure profiles from traversed data downstream of each row for a cold and hot day for the 3% TC
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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: TPR trends with measured rotor 1 TC at a near-stall operating condition
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Date of download: 11/6/2017 Copyright © ASME. All rights reserved. From: Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions J. Eng. Gas Turbines Power. 2015;137(12): doi: / Figure Legend: Radial profiles for three nominal TCs on a hot and cold day
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