Phase-locking condition in the feedback loop of low-speed edgetones

Journal of the Acoustical Society of America

Volumn 100, Issue 5, 1996, Pages 3028-3032

  Kwon, Young Pil ^a  

^a Soongsil University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTICS; ARTICLE; PRIORITY JOURNAL; SOUND; THEORY;

EID: 0029858336     PISSN: 00014966     EISSN: None     Source Type: Journal    
DOI: 10.1121/1.417114     Document Type: Article

References (10)

1. A. Powell, "On edge tones and associated phenomena," Acustica 3, 233-244 (1953).
2. G. B. Brown, "The vortex motion causing edge tones," Proc. Phys. Soc. London Ser. A 47, 493-507 (1935).
3. R. Kaykayoglu and D. Rockwell, "Unstable jet-edge interaction. Part 1. Instantaneous pressure fields at a single frequency," J. Fluid Mech. 169, 125-149 (1986).
4. D. K. Holger, T. A. Wilson, and G. S. Beavers, "Fluid mechanics of the Edgetone," J. Acoust. Soc. Am. 62, 1116-1128 (1977).
5. D. G. Crighton, "The jet-edge feedback cycle: Linear theory for the operating stages," J. Fluid Mech. 234, 361-391 (1992).
6. Y. P. Kwon and A. Powell, "A mechanism of jet-edge interaction and sound radiation," J. Acoust. Soc. Am. 92, 2310(A) (1992).
7. A. Powell and H. Unfried, "An experimental study of low-speed edgetones," University of California, Los Angeles, Report No. 64-49, 1964 (unpublished).
8. L. F. East, "Aerodynamically induced resonance in rectangular cavities," J. Sound Vib. 3(3), 277-287 (1966).
9. S. A. Elder, T. M. Farabee, and F. C. DeMetz, "Measurement of flow-excited cavitytones at low Mach number," J. Acoust. Soc. Am. 72, 532-549 (1982).
10. C. M. Ho and N. S. Nosseir, "Dynamics of a impinging jet. Part 1. The feedback phenomenon," J. Fluid Mech. 105, 119-142 (1981).