有翼阻塞喷注
THE CHOKED JET WITH A FOIL
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摘要: 冲击伴随噪声是阻塞喷注噪声的重要成分。通常认为它是由阻塞喷注中的大尺度湍流结构和冲击气室的相互作用所产生的,理论分析和有关的实验指出,在圆形喷口处加置翼片,将同时影响阻塞喷注中的冲击气室和大尺度湍流结构;有效地降低冲击伴随噪声。Abstract: The shock associated noise is an important component of choked jet noise, It is believed that the shock associated noise is emitted by the interaction between the large scale turbulent flow structures in the mixing layer of the jet and the shock cell system. Theoretical studies and experiments show the foil attached on a round nozzle affects the large scale turbulent flow structures as well as shock cell system, and reduces the shock associated noise.