Abstract

Turbulence parameters, in particular integral length scale (ILS) and turbulence intensity (Tu), are key input parameters for various applications in aerodynamics and aeroacoustics. The estimation of these parameters is typically performed using data obtained via hot-wire measurements. On the one hand, hot-wire measurements are affected by external disturbances resulting in increased measurement noise. On the other hand, commonly applied turbulence parameter estimators lack in robustness. If not addressed correctly, both issues may impede the accuracy of the turbulence parameter estimation. In this article, a procedure consisting of several signal processing steps is presented to filter non-turbulence related disturbances from the unsteady velocity data. The signal processing techniques comprise time- and frequency-domain approaches. For the turbulence parameter estimation, two different models of the turbulence spectra—the von Kármán model and the Bullen model—are fitted to match the spectrum of the measured data. The results of several parameter estimation techniques are compared. Computational Fluid Dynamics (CFD) data are used to validate the estimation techniques and also to assess the influence of the variation in window size on the estimated parameters. Additionally, hot-wire data from a high-speed fan rig are analyzed. ILS and Tu are assessed at several radial positions for two fan speeds. It is found that most techniques yield similar values for ILS and Tu. The comparison of the fitted spectra with the spectra of the measured data shows a good agreement in most cases provided that a sufficiently fine frequency resolution is applied. The ratio of ILS and Tu of the velocity components in longitudinal and transverse direction allows the assessment of flow-isotropy. Results indicate that the turbulence is anisotropic for the investigated flow fields.

Highlights

  • IntroductionThe pursuit for green solutions for the aircraft industry includes low greenhouse gas emissions, and quieter airplanes

  • The objective of this study is to identify the most suitable technique for the estimation of turbulence parameters, namely, the turbulence integral length scale and the turbulence intensity (which can be understood as a normalized turbulent kinetic energy (TKE))

  • The normalization of the spectra allows a comparison of all spectra from different measurement points, regardless of the velocity, turbulence level, and integral length scale

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Summary

Introduction

The pursuit for green solutions for the aircraft industry includes low greenhouse gas emissions, and quieter airplanes. Regulations and restrictions of aircraft noise emissions have become increasingly stringent over the past decades [1,2]. The engines of a modern aircraft are critical noise sources during approach and take-off [3,4]. In a modern Ultra-High By-pass Ratio (UHBR) turbofan engine, the fan stator interaction noise is the main contributor to the total engine noise emissions at both take-off and approach conditions. There is great interest from industry and the science to better understand fan noise mechanisms in order to develop solutions for quieter engines

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