Abstract

This paper investigates the application of flow-permeable materials as a solution for reducing jet-installation noise. Experiments are carried out with a flat plate placed in the near field of a single-stream subsonic jet. The flat plate is modular and the solid surface near the trailing edge can be replaced with different flow-permeable inserts, such as a metal foam and a perforated plate structure. The time-averaged jet flow field is characterized through planar PIV measurements at three different velocities (Ma=0.3,Ma=0.5 and Ma=0.8, where Ma is the acoustic Mach number), whereas the acoustic far-field is measured with a microphone arc-array. Acoustic measurements confirm that installation effects cause significant noise increase, up to 17 dB for the lowest jet velocity, particularly at low and mid frequencies (i.e. St<0.7, with the Strouhal number based on the jet diameter and velocity), and mostly in the upstream direction of the jet. By replacing the solid trailing edge with the metal foam, noise abatement of up to 9 dB is achieved at the spectral peak for Ma=0.3 and a polar angle θ=40∘, with an overall reduction in the entire frequency range where jet-installation noise is dominant. The perforated plate provides lower noise reduction than the metal foam (7 dB at the spectral peak for Ma=0.3 and θ=40∘), and it is less effective at low frequencies. This is related to the values of permeability and form coefficient of the materials, which are the major parameters controlling the pressure balance across the trailing edge and, consequently, the noise generated by the plate. However, despite having a high permeability, the plate with the metal-foam trailing edge still has a distinct noise production at mid frequencies (St≈0.43 for Ma=0.3). Based on the analyses of different treated surface lengths, it is conjectured that the solid-permeable junction in the plate acts as a new scattering region, and thus its position also affects the far-field noise, which is in line with analytical predictions in the literature. Nonetheless, both types of inserts provide significant noise reduction and are potential solutions for the problem of jet-installation noise.

Highlights

  • Jet-installation noise (JIN) arises from the interaction between the exhaust flow of an aircraft jet engine and a nearby airframe surface [1,2]

  • The Particle Image Velocimetry (PIV) measurements are performed for the 3 investigated acoustic Mach numbers and the results are displayed in terms of time-averaged axial velocity u and the r.m.s. of velocity fluctuations

  • The results show that at this height and for Ma = 0.3, for example, noise reductions up to 10 dB and 6 dB with respect to the solid case are achieved for the metal foam and perforated plate, respectively, for St = 0.37

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Summary

Introduction

Jet-installation noise (JIN) arises from the interaction between the exhaust flow of an aircraft jet engine and a nearby airframe surface [1,2]. For the case of an installed subsonic jet, aside from the turbulence-mixing noise component, there is an additional source at the surface trailing edge [3]. This region acts as a singularity for convecting hydrodynamic pressure waves, which are generated by the jet mixing-layer, resulting in their scattering as noise. This phenomenon is responsible for noise increase at low and mid frequencies, in the directions normal and upstream of the jet axis, equivalent to a distribution of acoustic dipoles at the trailing edge [4,5,6]. The development of noise reduction solutions for this particular source is of interest

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