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The effects of inlet conditions on supersonic cascade noise

โœ 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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โœฆ 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.


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EFFECTS OF CHOKING ON THE AEROACOUSTICS
โœ K.C. Miller; W.F. Ng ๐Ÿ“‚ Article ๐Ÿ“… 1997 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 203 KB

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 10โ€ข4 cm