The effects of inlet conditions on supersonic cascade noise
โ Scribed by D.L. Hawkings
- Publisher
- Elsevier Science
- Year
- 1974
- Tongue
- English
- Weight
- 865 KB
- Volume
- 33
- Category
- Article
- ISSN
- 0022-460X
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โฆ Synopsis
A theory is presented describing the generation of noise by supersonic cascades with non-uniform inlet ducts. The analysis is based upon a quasi-two-dimensional model, and allows for a slow variation of duct cross-sectional area and axial velocity upstream of the blades. The technique used is a combination of geometric acoustics and weak shock theory. It is shown that the upstream acoustic field depends primarily upon a single age parameter which is defined by a simple integral of the duct area and velocity distributions. The general implications for minimising the noise output are explained, and two numerical examples are also given.
๐ SIMILAR VOLUMES
An experimental study was conducted to determine the effect of choking on the aerodynamic and acoustic performance of a supersonic inlet. The investigated inlet was a prototype model of a mixed compression, axisymmetric supersonic inlet designed for the high speed civil transport aircraft. A 10โข4 cm