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Elimination of screech tone noise in supersonic swirling jets
被引:3
|作者:
Chen, RH
[1
]
Yu, YK
[1
]
机构:
[1] Univ Cent Florida, Dept Mech Mat & Aerosp Engn, Orlando, FL 32816 USA
关键词:
D O I:
10.2514/2.7559
中图分类号:
V [航空、航天];
学科分类号:
08 ;
0825 ;
摘要:
Imparting a sufficient degree of swirl in underexpanded jets issuing from a convergent nozzle eliminates the quasiperiodic shock cells downstream of the third shock cell, which is also downstream of the flow recirculation zone. Since the existence of the fourth and the fifth shock cells is responsible for the screech tone noise generation, imparting swirl to a supersonic jet can eliminate screech tone noise. Flow recirculation alone does not eliminate the quasiperiodic shock cell structure downstream of the third shock cell. Swirl helps to eliminate the quasiperiodic shock cell structure that is essential for screech tone noise generation.
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页码:998 / 1000
页数:3
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