Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions

Author:

Smith Natalie R.1,Berdanier Reid A.2,Fabian John C.2,Key Nicole L.3

Affiliation:

1. Department of Aeronautics and Astronautics, Purdue University, 500 Allison Road, West Lafayette, IN 47907 e-mail:

2. Department of Mechanical Engineering, Purdue University, 500 Allison Road, West Lafayette, IN 47907 e-mail:

3. Associate Professor Department of Mechanical Engineering, Purdue University, 500 Allison Road, West Lafayette, IN 47907 e-mail:

Abstract

Careful experimental measurements can capture small changes in compressor total pressure ratio (TPR), which arise with subtle changes in an experiment's configuration. Research facilities that use unconditioned atmospheric air must account for changes in ambient compressor inlet conditions to establish repeatable performance maps. A unique dataset from a three-stage axial compressor has been acquired over the duration of 12 months in the Midwest U.S., where ambient conditions change significantly. The trends show a difference in compressor TPR measured on a cold day versus a warm day despite correcting inlet conditions to sea level standard day. To reconcile these differences, this paper explores correcting the compressor exit thermodynamic state, Reynolds number effects, and variations in rotor tip clearance (TC) as a result of differences in thermal growth.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference26 articles.

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2. Bird, J., and Grabe, W., 1991, “Humidity Effects on Gas Turbine Performance,” International Gas Turbine and Aeroengine Congress and Exposition, Orlando, FL, June 3–6, ASME Paper No. 91-GT-32910.1115/91-GT-329.

3. Humidity Effects on Experimental Compressor Performance—Corrected Conditions for Real Gases;ASME J. Turbomach.,2015

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