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Volumn 382, Issue , 1999, Pages 27-61

Boundary-layer instability noise on aerofoils

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; FLOW VISUALIZATION; REYNOLDS NUMBER; VELOCITY MEASUREMENT; WIND TUNNELS;

EID: 0032687858     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S002211209800367X     Document Type: Article
Times cited : (264)

References (42)
  • 1
    • 0344025409 scopus 로고
    • Sound generation by a Tollmien-Schlichting wave at the end of a plate in a flow
    • AIZIN, L. B. 1992 Sound generation by a Tollmien-Schlichting wave at the end of a plate in a flow. Prikl. Mekh. Tekh. Fiz. 3, 50-57.
    • (1992) Prikl. Mekh. Tekh. Fiz. , vol.3 , pp. 50-57
    • Aizin, L.B.1
  • 2
    • 32944465517 scopus 로고
    • Tone-like noise from an isolated two dimensional aerofoil
    • AKISHITA, S. 1986 Tone-like noise from an isolated two dimensional aerofoil. AIAA paper 86-1947.
    • (1986) AIAA Paper 86-1947
    • Akishita, S.1
  • 3
    • 0020814501 scopus 로고
    • Noise generated by airfoil profiles placed in a uniform laminar flow
    • ARBEY, H. & BATAILLE, J. 1983 Noise generated by airfoil profiles placed in a uniform laminar flow. J. Fluid Mech. 134, 33-47.
    • (1983) J. Fluid Mech. , vol.134 , pp. 33-47
    • Arbey, H.1    Bataille, J.2
  • 4
    • 0016845831 scopus 로고
    • The laminar boundary layer instability excitation of an acoustic resonance
    • ARCHIBALD, F. S. 1975a The laminar boundary layer instability excitation of an acoustic resonance. J. Sound Vib. 38, 387-402.
    • (1975) J. Sound Vib. , vol.38 , pp. 387-402
    • Archibald, F.S.1
  • 5
    • 0016522023 scopus 로고
    • Unsteady Kutta condition at high values of the reduced frequency parameter
    • ARCHIBALD, F. S. 1975b Unsteady Kutta condition at high values of the reduced frequency parameter. J. Aircraft 12, 545-550.
    • (1975) J. Aircraft , vol.12 , pp. 545-550
    • Archibald, F.S.1
  • 6
    • 0021394102 scopus 로고
    • Design and performance of a new low turbulence wind tunnel at Bristol University
    • BARRETT, R. V. 1984 Design and performance of a new low turbulence wind tunnel at Bristol University. Aeronaut. J. 88, 86-90.
    • (1984) Aeronaut. J. , vol.88 , pp. 86-90
    • Barrett, R.V.1
  • 7
    • 0032091610 scopus 로고    scopus 로고
    • Realisation of the full potential of the laser Doppler anemometer in the analysis of complex flows
    • BARRETT, R. V. & SWALES, C. S. 1998 Realisation of the full potential of the laser Doppler anemometer in the analysis of complex flows. Aeronaut. J. 102, 313-320.
    • (1998) Aeronaut. J. , vol.102 , pp. 313-320
    • Barrett, R.V.1    Swales, C.S.2
  • 9
    • 0015144161 scopus 로고
    • The radiation of sound from an airfoil immersed in a laminar flow
    • CLARK, L. T. 1971 The radiation of sound from an airfoil immersed in a laminar flow. Trans ASME A: J. Engng Power 93, 366-376.
    • (1971) Trans ASME A: J. Engng Power , vol.93 , pp. 366-376
    • Clark, L.T.1
  • 11
    • 0022182220 scopus 로고
    • Development of Vortical Disturbances in Flow with Laminar Separation
    • Springer
    • DOVGAL, A. V. 1985 Development of Vortical Disturbances in Flow with Laminar Separation. Proc. IUTAM Symp. Laminar-Turbulent Transition, pp. 359-366, Springer.
    • (1985) Proc. IUTAM Symp. Laminar-Turbulent Transition , pp. 359-366
    • Dovgal, A.V.1
  • 12
    • 0020715216 scopus 로고
    • Influence of acoustic perturbations on the flow structure in a boundary layer with adverse pressure gradient
    • trans. from Russian
    • DOVGAL, A. V. & KOZLOV, V. V. 1983 Influence of acoustic perturbations on the flow structure in a boundary layer with adverse pressure gradient. Fluid Dyn. 18, 205-209 (trans. from Russian).
    • (1983) Fluid Dyn. , vol.18 , pp. 205-209
    • Dovgal, A.V.1    Kozlov, V.V.2
  • 13
    • 0002545220 scopus 로고
    • Laminar boundary layer separation: Instability and associated phenomena
    • DOVGAL, A. V., KOZLOV, V. V. & MICHALKE, A. 1994 Laminar boundary layer separation: instability and associated phenomena. Prog. Aerospace Sci. 30, 61-94.
    • (1994) Prog. Aerospace Sci. , vol.30 , pp. 61-94
    • Dovgal, A.V.1    Kozlov, V.V.2    Michalke, A.3
  • 14
    • 0001520256 scopus 로고
    • Some approximate solutions of the boundary layer equations
    • FALKNER, V. M. & SKAN, S. W. 1931 Some approximate solutions of the boundary layer equations. Phil. Mag. 12, 865.
    • (1931) Phil. Mag. , vol.12 , pp. 865
    • Falkner, V.M.1    Skan, S.W.2
  • 15
    • 0014937763 scopus 로고
    • Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane
    • FFOWCS WILLIAMS, J. E. & HALL, L. H. 1970 Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane. J. Fluid Mech. 40, 657-670.
    • (1970) J. Fluid Mech. , vol.40 , pp. 657-670
    • Ffowcs Williams, J.E.1    Hall, L.H.2
  • 16
    • 0347526529 scopus 로고
    • Fine structure of airfoil tone frequency
    • Paper H3 presented
    • FINK, M. R. 1978 Fine structure of airfoil tone frequency. Paper H3 presented at the 95th Meeting Acoust. Soc. Amer.
    • (1978) 95th Meeting Acoust. Soc. Amer.
    • Fink, M.R.1
  • 19
    • 0042217654 scopus 로고
    • The structure and behaviour of laminar separation bubbles
    • GASTER, M. 1966 The structure and behaviour of laminar separation bubbles. AGARD Conf. Proc. 4, Separated Flows, 813-854.
    • (1966) AGARD Conf. Proc. 4, Separated Flows , vol.4 , pp. 813-854
    • Gaster, M.1
  • 20
    • 0000245555 scopus 로고
    • Streaklines in perturbd shear flow
    • HAMA, F. R. 1962 Streaklines in perturbd shear flow. Phys. Fluids 5, 644-650.
    • (1962) Phys. Fluids , vol.5 , pp. 644-650
    • Hama, F.R.1
  • 21
    • 84958735159 scopus 로고
    • On an equation occurring in Falkner and Skans's approximate treatment of the equations of the boundary layer
    • HARTREE, D. R. 1937 On an equation occurring in Falkner and Skans's approximate treatment of the equations of the boundary layer. Proc. Camb. Phil. Soc. 33, 223.
    • (1937) Proc. Camb. Phil. Soc. , vol.33 , pp. 223
    • Hartree, D.R.1
  • 25
    • 0017769762 scopus 로고
    • Vortex shedding of low tip speed, axial flow fans
    • LONGHOUSE, R. E. 1977 Vortex shedding of low tip speed, axial flow fans. J. Sound Vib. 53, 25-46.
    • (1977) J. Sound Vib. , vol.53 , pp. 25-46
    • Longhouse, R.E.1
  • 28
    • 0345319517 scopus 로고    scopus 로고
    • On the generation of discrete frequency tones by the flow around an aerofoil
    • to be published
    • MCALPINE, A., NASH, E. C. & LOWSON, M. V. 1999 On the generation of discrete frequency tones by the flow around an aerofoil. J. Sound Vib. (to be published).
    • (1999) J. Sound Vib.
    • Mcalpine, A.1    Nash, E.C.2    Lowson, M.V.3
  • 29
    • 0344025401 scopus 로고
    • Experimental study of noise generated in a low-velocity flow
    • Jan-Feb. 1992
    • MUNIN, A. G., PROZOROV, A. G. & TOPOROV, A. V. 1992 Experimental study of noise generated in a low-velocity flow. Sov. Phys. Acoust. 38, Jan-Feb. 1992.
    • (1992) Sov. Phys. Acoust. , vol.38
    • Munin, A.G.1    Prozorov, A.G.2    Toporov, A.V.3
  • 30
    • 0344888346 scopus 로고    scopus 로고
    • PhD thesis, Department of Aerospace Engineering, University of Bristol
    • NASH, E. C. 1996 Boundary layer instability noise on aerofoils. PhD thesis, Department of Aerospace Engineering, University of Bristol.
    • (1996) Boundary Layer Instability Noise on Aerofoils
    • Nash, E.C.1
  • 31
    • 0012615577 scopus 로고
    • Noise due to boundary layer instabilities
    • Paper CEAS/AIAA-95-124, Munich
    • NASH, E. C. & LOWSON, M. V. 1995 Noise due to boundary layer instabilities. Paper CEAS/AIAA-95-124, CEAS/AIAA Aeroacoustics Conference, Munich.
    • (1995) CEAS/AIAA Aeroacoustics Conference
    • Nash, E.C.1    Lowson, M.V.2
  • 32
    • 0002821602 scopus 로고    scopus 로고
    • Resonance effects in wake shedding from parallel plates: Some experimental observations
    • PARKER, R. 1996 Resonance effects in wake shedding from parallel plates: Some experimental observations. J. Sound Vib. 4, 62-72.
    • (1996) J. Sound Vib. , vol.4 , pp. 62-72
    • Parker, R.1
  • 33
    • 49949140692 scopus 로고    scopus 로고
    • Resonance effects in wake shedding from parallel plates: Calculation of resonant frequencies
    • PARKER, R. 1997 Resonance effects in wake shedding from parallel plates: calculation of resonant frequencies. J. Sound Vib. 5, 330-343.
    • (1997) J. Sound Vib. , vol.5 , pp. 330-343
    • Parker, R.1
  • 36
    • 0344025400 scopus 로고
    • Calculated amplified oscillations in the plane Poiseuille and Blasius flows
    • SHEN, S. F. 1954 Calculated amplified oscillations in the plane Poiseuille and Blasius flows. J. Aeronaut. Sci. Readers Forum, 62-64.
    • (1954) J. Aeronaut. Sci. Readers Forum , pp. 62-64
    • Shen, S.F.1
  • 37
    • 0022075598 scopus 로고
    • An inverse boundary element method for single component aircraft design
    • SOINNE, E. & LAINE, S. 1988 An inverse boundary element method for single component aircraft design. J. Aircraft 22, 541-543.
    • (1988) J. Aircraft , vol.22 , pp. 541-543
    • Soinne, E.1    Laine, S.2
  • 38
    • 0344025399 scopus 로고
    • Correlations between far field acoustic pressure and flow characteristics for a single airfoil
    • Noise Mechanisms, Paper 5
    • SUNYACH, M., ARBEY, H., ROBERT, D., BATAILLE, J. & COMTE-BELLOT, G. 1973 Correlations between far field acoustic pressure and flow characteristics for a single airfoil. AGARD Conf. Proc. 131, Noise Mechanisms, Paper 5.
    • (1973) AGARD Conf. Proc. , vol.131
    • Sunyach, M.1    Arbey, H.2    Robert, D.3    Bataille, J.4    Comte-Bellot, G.5
  • 41
    • 0016072743 scopus 로고
    • Discrete tones of isolated airfoils
    • TAM, C. K. W. 1974 Discrete tones of isolated airfoils. J. Acoust. Soc. Am. 55, 6.
    • (1974) J. Acoust. Soc. Am. , vol.55 , pp. 6
    • Tam, C.K.W.1
  • 42
    • 0016934963 scopus 로고
    • The acoustic spectrum of axial flow machines
    • WRIGHT, S. E. 1976 The acoustic spectrum of axial flow machines. J. Sound Vib. 45, 165-223.
    • (1976) J. Sound Vib. , vol.45 , pp. 165-223
    • Wright, S.E.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.