Spatial Flow-Field Approximation Using Few Thermodynamic Measurements—Part I: Formulation and Area Averaging

Author:

Seshadri Pranay12,Simpson Duncan3,Thorne George3,Duncan Andrew42,Parks Geoffrey1

Affiliation:

1. Department of Engineering, University of Cambridge, Cambridge CB2 1PZ, UK

2. Data-Centric Engineering, The Alan Turing Institute, London NW1 2DB, UK

3. Civil Aerospace, Rolls-Royce plc, Derby DE24 8BJ, UK

4. Department of Mathematics, Imperial College London, London SW7 2AZ, UK

Abstract

Abstract Our investigation raises an important question that is of relevance to the wider turbomachinery community: how do we estimate the spatial average of a flow quantity given finite (and sparse) measurements? This paper seeks to advance efforts to answer this question rigorously. In this paper, we develop a regularized multivariate linear regression framework for studying engine temperature measurements. As part of this investigation, we study the temperature measurements obtained from the same axial plane across five different engines yielding a total of 82 datasets. The five different engines have similar architectures and therefore similar temperature spatial harmonics are expected. Our problem is to estimate the spatial field in engine temperature given a few measurements obtained from thermocouples positioned on a set of rakes. Our motivation for doing so is to understand key engine temperature modes that cannot be captured in a rig or in computational simulations, as the cause of these modes may not be replicated in these simpler environments. To this end, we develop a multivariate linear least-squares model with Tikhonov regularization to estimate the 2D temperature spatial field. Our model uses a Fourier expansion in the circumferential direction and a quadratic polynomial expansion in the radial direction. One important component of our modeling framework is the selection of model parameters, i.e., the harmonics in the circumferential direction. A training-testing paradigm is proposed and applied to quantify the harmonics.

Publisher

ASME International

Subject

Mechanical Engineering

Reference20 articles.

1. Analysis of Rotor–Stator-Interaction and Blade-to-Blade Measurements in a Two Stage Axial Flow Compressor;Ernst;ASME J. Turbomach.,2011

2. Multi-Blade Row Interactions in a Transonic Axial Compressor: Part I—Stator Particle Image Velocimetry (PIV) Investigation;Sanders;ASME J. Turbomach.,2002

3. Periodical Unsteady Flow Within a Rotor Blade Row of an Axial Compressor Part I: Flow Field at Midspan;Mailach;ASME J. Turbomach.,2008

4. Stoll, F., Tremback, J. W., and Arnaiz, H. H., 1979, “Effect of Number of Probes and Their Orientation on the Calculation of Several Compressor Face Distortion Descriptors,” Tech. rep., NASA Technical Memorandum 72859.

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