Experimental and Theoretical Investigations of Edge Tones in High Speed Jets
Author:
Affiliation:
1. Aerospace Engineering Department Faculty of Engineering, University of Cairo
Publisher
Japan Society of Mechanical Engineers
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering
Link
https://www.jstage.jst.go.jp/article/jfst/8/1/8_1/_pdf
Reference21 articles.
1. Theoretical model of discrete tone generation by impinging jets
2. On the Edgetone
3. (3) J. P. Woolley and K. Karamcheti. A study of narrow band noise generation by flow over ventilated walls in transonic wind tunnels. Technical Report TR-73-0503, AFOSR, 1973.
4. Flow field and noise characteristics of a supersonic impinging jet
5. (5) Praveen Panicker and Ganesh Raman. Criteria for the existance of helical instabilities in subsonic impinging jets. Physics of Fluids, 19: 106103, 2007.
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