An experiment was conducted on a two-dimensional bifurcated, supersonic inlet to investigate the aeroacoustics at take-o! and landing conditions. A 104)1 mm (4)1 in) diameter turbofan simulator was coupled to the inlet to generate the noise typical of a turbofan engine. Aerodynamic and acoustic data
Aeroacoustics of T-junctions—An experimental investigation
✍ Scribed by Mikael Karlsson; Mats Åbom
- Publisher
- Elsevier Science
- Year
- 2010
- Tongue
- English
- Weight
- 858 KB
- Volume
- 329
- Category
- Article
- ISSN
- 0022-460X
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✦ Synopsis
An experimental method for determining the aeroacoustic properties of side branch orifices allowing for any combination of grazing and bias flow is presented. The geometry studied, a T-junction, is treated as an active acoustic three-port. The passive properties, describing the reflection and transmission of an incident acoustic wave, are described by a system matrix while the active properties are described by a source vector. Expressions for the acoustic impedance under various mean flow and acoustic incidence configurations are developed. In addition, methods for identifying regions where the system can generate sound, by studying only the passive properties, are discussed. A self-sustained oscillation is triggered at one of the identified regions by coupling a resonant system to the three-port.
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