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Showing 1 to 13 of 13 for “"acoustic liners"”.

  1. Numerical investigation of slat noise attenuation using acoustic liners

    … of attenuating slat noise using absorptive acoustic liners in the slat/main element gap is explored using a time domain computational aeroacoustic (CAA) technique. The aims of the development and application of the computational method are to reveal the mechanism of the slat noise generation …

    soton Repository record for Numerical investigation of slat noise attenuation using acoustic liners (opens in a new tab)

  2. Direct numerical investigation and reduced-order modeling of 3-D honeycomb acoustic liners

    Single degree-of-freedom conventional acoustic liners are widely installed in jet engines to reduce internal engine noise. They work by converting acoustic energy into vorticity-bound fluctuations. Despite being widely used, effective design-stage models of acoustic liners placed in high sound …

    uiuc Repository record for Direct numerical investigation and reduced-order modeling of 3-D honeycomb acoustic liners (opens in a new tab)

  3. Damping Parameter Study of a Perforated Plate with Bias Flow

    … is the dynamic instability also known as thermo-acoustic instability. Concerns with this ongoing problem have grown with the introduction of Lean Premixed Combustion (LPC) systems developed to address the environmental concerns associated with the conventional combustion systems.</p><p>The most …

    ohiolink Repository record for Damping Parameter Study of a Perforated Plate with Bias Flow (opens in a new tab)

  4. Investigating the Feasibility and Stability for Modeling Acoustic Wave Scattering Using a Time-Domain Boundary Integral Equation with Impedance Boundary Condition

    … objective in the field of computational aeroacoustics. When designing next generation quiet and environmentally friendly aircraft, it is important to be able to accurately and efficiently predict the acoustic scattering by an aircraft body from a given noise source. Acoustic liners are an …

    odu Repository record for Investigating the Feasibility and Stability for Modeling Acoustic Wave Scattering Using a Time-Domain Boundary Integral Equation with Impedance Boundary Condition (opens in a new tab)

  5. Improvement In Acoustic Liner Attenuation In Turbofan Engines By Means Of Plasma Synthetic Jet Actuator

    … to reduce noise emissions. Turbofan engine acoustic liners are efficient attenuators of engine noise. Plasma actuators have been used as flow control devices in other settings and will now be studied as an enhancement for acoustic liners. A plasma actuator can excite oscillatory flow or a …

    vt Repository record for Improvement In Acoustic Liner Attenuation In Turbofan Engines By Means Of Plasma Synthetic Jet Actuator (opens in a new tab)

  6. Theoretical Modeling with Validation of a Combined HQ-Liner System for Turbofan Engine Noise Control

    The combination of traditional passive acoustic liners with Herschel-Quincke (HQ) waveguides is proposed in this work as a device for Turbofan Engine Noise Control. The approach consists of installing circumferential arrays of HQ tubes on the lined sector of the inlet of a turbofan engine. A …

    vt Repository record for Theoretical Modeling with Validation of a Combined HQ-Liner System for Turbofan Engine Noise Control (opens in a new tab)

  7. Advanced Trailing Edge Blowing Concepts for Fan Noise Control: Experimental Validation

    … spectral shape increases the performance of acoustic liners used in conjunction with trailing edge blowing. This thesis presents numerical predictions performed to estimate the sound power reductions due to these concepts, as well as experimental results taken on the ANCF rig at NASA Glenn …

    vt Repository record for Advanced Trailing Edge Blowing Concepts for Fan Noise Control: Experimental Validation (opens in a new tab)

  8. Acoustic and thermal packaging of small gas turbines for portable power

    … gas turbine engine poses major challenges in the acoustic treatment that is required to attenuate the broadband and tonal noise of the high-speed turbomachinery. The challenge in the thermal management is the relatively large required cooling mass flow and the short flow mixing length, constrained …

    mit Repository record for Acoustic and thermal packaging of small gas turbines for portable power (opens in a new tab)

  9. Acoustic optimisation and prediction of sound propagation in turbofan engine ducts

    … optimisation of noise attenuation<br/>by using acoustic liners. A commercial FE/IE code ACTRAN/TM is used<br/>within two shell programs; B-induct for bypass ducts and ANPRORAD for intake ducts.<br/><br/>An automated liner impedance capability has been demonstrated by exploiting an …

    soton Repository record for Acoustic optimisation and prediction of sound propagation in turbofan engine ducts (opens in a new tab)

  10. Experiments and Impedance Modeling of Liners Including The Effect of Bias Flow

    The study of normal impedance of perforated plate acoustic liners including the effect of bias flow was studied. Two impedance models were developed, by modeling the internal flows of perforate orifices as infinite tubes with the inclusion of end corrections to handle finite length effects. These …

    vt Repository record for Experiments and Impedance Modeling of Liners Including The Effect of Bias Flow (opens in a new tab)

  11. Broadband Acoustic Liner Optimization Study Using Novel Poro-elastic Materials

    … aircraft engine noise, there is need for acoustic liner configurations that target broadband performance. This thesis experimentally and analytically investigates passive noise control methods to improve broadband frequency attenuation through various acoustic liner designs. The inclusion …

    vt Repository record for Broadband Acoustic Liner Optimization Study Using Novel Poro-elastic Materials (opens in a new tab)

  12. Prediction and control of sound propagation in turbofan engine bypass ducts

    … research into the propagation of sound in acoustically lined ducts<br/>with flow. The motivation for this work is the requirement to predict the sound attenuation of<br/>acoustic liners in the bypass duct of modern turbofan aeroengines. The liners provide the most<br/>effective means with …

    soton Repository record for Prediction and control of sound propagation in turbofan engine bypass ducts (opens in a new tab)