A Stochastic Model for a Compressor Stability Measure

Author:

Dhingra Manuj1,Neumeier Yedidia1,Prasad J. V. R.1,Breeze-Stringfellow Andrew2,Shin Hyoun-Woo2,Szucs Peter N.2

Affiliation:

1. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332

2. GE Aviation, Cincinnati, OH 45215

Abstract

A stability measure rooted in the unsteady characteristics of the flow field over the compressor rotor has been previously developed. The present work explores the relationship between the stochastic properties of this measure, called the correlation measure, and the compressor stability boundary. A stochastic model has been developed to gauge the impact of the correlation measure’s stochastic nature on its applicability to compressor stability management. The genesis of this model is in the fundamental properties of a specific stochastic process, one that is created by the threshold crossings of a random process. The model validation utilizes data obtained on three different axial compressor facilities. These include a single-stage low-speed axial compressor, a four-stage low-speed research compressor, and an advanced technology demonstrator high-speed compressor. This paper presents details of the model development and validation, as well as closed loop experimental results to demonstrate correlation measure’s usefulness in compressor stability management.

Publisher

ASME International

Subject

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

Reference21 articles.

1. Theory of Post Stall Transients in Axial Compression Systems—Part I: Development of Equations;Moore;Trans. ASME: J. Eng. Gas Turbines Power

2. Theory of Post Stall Transients in Axial Compression Systems—Part II: Application;Moore;Trans. ASME: J. Eng. Gas Turbines Power

3. Active Suppression of Aerodynamic Instabilities in Turbomachines;Epstein;J. Propul. Power

4. Active Stabilization of Rotating Stall and Surge in a Transonic Single-Stage Axial Compressor;Weigl;J. Turbomach.

5. Simplified Approach for Control of Rotating Stall—Part 1: Theoretical Development;Badmus;J. Propul. Power

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