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Volumn 48, Issue 2, 2005, Pages 342-349

Experimental investigation on surface impedance effect of sound radiation from low mach number flow around a circular cylinder

Author keywords

Aerodynamic acoustics; Boundary conditions; Karman vortex flow; Surface impedance; Wind tunnel experiment

Indexed keywords

ACOUSTIC SURFACE WAVE DEVICES; ACOUSTIC WAVES; HYDRODYNAMICS; PRESSURE CONTROL; REYNOLDS NUMBER; WIND TUNNELS;

EID: 21944431552     PISSN: 13408054     EISSN: None     Source Type: Journal    
DOI: 10.1299/jsmeb.48.342     Document Type: Article
Times cited : (17)

References (7)
  • 1
    • 0018781805 scopus 로고
    • On the Added Mass of a Perforated Shell, with Application to the Generation of Aerodynamic Sound by a Perforated Trailing Edge
    • Howe, M.S., On the Added Mass of a Perforated Shell, with Application to the Generation of Aerodynamic Sound by a Perforated Trailing Edge, Proceedings of the Royal Society, A, Vo1.365 (1979), pp.209-233.
    • (1979) Proceedings of the Royal Society, A , vol.365 , pp. 209-233
    • Howe, M.S.1
  • 2
    • 32644482662 scopus 로고
    • Exploratory Investigation of Aeroacoustic Optimization of the Variable Impedance Edge Concept Applied to Upper Surface Blown Configuration
    • NASA CR-145072, Nov
    • Hayden, R.E., Exploratory Investigation of Aeroacoustic Optimization of the Variable Impedance Edge Concept Applied to Upper Surface Blown Configuration, NASA CR-145072, Nov., (1976).
    • (1976)
    • Hayden, R.E.1
  • 3
    • 1842689686 scopus 로고    scopus 로고
    • Investigation on the Effect of Surface Impedance for Reducing Aerodynamic Sound from Circular Cylinder
    • Ser. B
    • Yahathugoda, I. and Akishita, S., Investigation on the Effect of Surface Impedance for Reducing Aerodynamic Sound from Circular Cylinder, JSME Int. J., Ser. B, Vol.2, No.1 (2004), pp.67-74.
    • (2004) JSME Int. J. , vol.2 , Issue.1 , pp. 67-74
    • Yahathugoda, I.1    Akishita, S.2
  • 5
    • 1842727174 scopus 로고    scopus 로고
    • Study on Exploring the Function of Functional Acoustic Boundary by Using MEMS
    • (in Japanese), Doctoral Thesis, Faculty of Science and Engineering, Ritsumeikan University
    • Yoda, M., Study on Exploring the Function of Functional Acoustic Boundary by Using MEMS, (in Japanese), Doctoral Thesis, Faculty of Science and Engineering, Ritsumeikan University, (2001).
    • (2001)
    • Yoda, M.1
  • 6
    • 84982318948 scopus 로고    scopus 로고
    • Model for the Control of Sound Radiation from an Aircraft Panel Excited by a Turbulent Boundary Layer Using Impedance Control
    • Curtis, R.D. and Remington, P.J., Model for the Control of Sound Radiation from an Aircraft Panel Excited by a Turbulent Boundary Layer Using Impedance Control, Proceedings of 5th AIAA/CEAS Aeroacoustics Conference, Vol.2 (1999), pp.882-890.
    • (1999) Proceedings of 5th AIAA/CEAS Aeroacoustics Conference , vol.2 , pp. 882-890
    • Curtis, R.D.1    Remington, P.J.2
  • 7
    • 32644470693 scopus 로고    scopus 로고
    • Active Control of Liner Impedance by Varying Perforate Orifice Geometry
    • NASA CR-2000-210633, Dec
    • Ahuja, K.K. and Gaeta, R.J., Jr., Active Control of Liner Impedance by Varying Perforate Orifice Geometry, NASA CR-2000-210633, Dec., (2000).
    • (2000)
    • Ahuja, K.K.1    Gaeta Jr., R.J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.