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Volumn 330, Issue 17, 2011, Pages 4114-4122

Adjoint-based optimization for understanding and suppressing jet noise

Author keywords

[No Author keywords available]

Indexed keywords

ADJOINT SYSTEM; ADJOINT-BASED OPTIMIZATION; ADJOINTS; ADVANCED SIMULATION; AIRCRAFT NOISE; COMPUTATIONAL COSTS; COMPUTER RESOURCES; DESIGN GUIDANCE; DESIGN IMPROVEMENTS; DESIGN OPTIMIZATION; FLOW CONDITION; GRADIENT INFORMATIONS; JET NOISE; KEY FACTORS; NOZZLE GEOMETRIES; QUALITY PREDICTION; SIMULATION TECHNIQUE; TURBULENT JET;

EID: 79957967227     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/j.jsv.2011.02.009     Document Type: Conference Paper
Times cited : (45)

References (35)
  • 1
    • 19644375797 scopus 로고    scopus 로고
    • Parametric testing of chevrons on single flow hot jets
    • J. Bridges, C.A. Brown, Parametric testing of chevrons on single flow hot jets, AIAA Paper 2004-2824, 2004.
    • (2004) AIAA Paper 2004-2824
    • Bridges, J.1    Brown, C.A.2
  • 2
    • 38549100649 scopus 로고    scopus 로고
    • Near-field investigation of chevron nozzle mechanisms
    • DOI 10.2514/1.17720
    • B. Callender, E. Gutmark, and S. Martens Near-field investigation of chevron nozzle mechanisms AIAA Journal 46 1 2008 36 45 (Pubitemid 351158399)
    • (2008) AIAA Journal , vol.46 , Issue.1 , pp. 36-45
    • Callender, B.1    Gutmark, E.2    Martens, S.3
  • 3
    • 71049142172 scopus 로고    scopus 로고
    • Control of a high Reynolds number Mach 0.9 heated jet using plasma actuators
    • M. Kearney-Fischer, J.-H. Kim, and M. Samimy Control of a high Reynolds number Mach 0.9 heated jet using plasma actuators Physics of Fluids 21 2009 095101
    • (2009) Physics of Fluids , vol.21 , pp. 095101
    • Kearney-Fischer, M.1    Kim, J.-H.2    Samimy, M.3
  • 4
    • 34247492824 scopus 로고    scopus 로고
    • Active control of a Mach 0.9 jet for noise mitigation using plasma actuators
    • DOI 10.2514/1.27499
    • M. Samimy, J.-H. Kim, J. Kastner, I. Adamovich, and Y. Utkin Active control of a Mach 0.9 jet for noise mitigation using plasma actuators AIAA Journal 45 4 2007 890 901 (Pubitemid 46646801)
    • (2007) AIAA Journal , vol.45 , Issue.4 , pp. 890-901
    • Samimy, M.1    Kim, J.-H.2    Kastner, J.3    Adamovich, I.4    Utkin, Y.5
  • 7
    • 0001420161 scopus 로고
    • On sound generated aerodynamically: II. Turbulence as a source of sound
    • M.J. Lighthill On sound generated aerodynamically: II. Turbulence as a source of sound Proceedings of the Royal Society of London A 222 1954 1 32
    • (1954) Proceedings of the Royal Society of London A , vol.222 , pp. 1-32
    • Lighthill, M.J.1
  • 9
    • 0041856452 scopus 로고    scopus 로고
    • A generalized acoustic analogy
    • DOI 10.1017/S0022112003004890
    • M.E. Goldstein A generalized acoustic analogy Journal of Fluid Mechanics 488 2003 315 333 (Pubitemid 37060676)
    • (2003) Journal of Fluid Mechanics , vol.488 , pp. 315-333
    • Goldstein, M.E.1
  • 10
    • 0032164611 scopus 로고    scopus 로고
    • Mean flow refraction effects on sound radiated from localized sources in a jet
    • C.K.W. Tam, and L. Auriault Mean flow refraction effects on sound radiated from localized sources in a jet Journal of Fluid Mechanics 370 1998 149 174 (Pubitemid 128490026)
    • (1998) Journal of Fluid Mechanics , vol.370 , pp. 149-174
    • Tam, C.K.W.1    Auriault, L.2
  • 11
    • 33751251013 scopus 로고    scopus 로고
    • Robustness of acoustic analogies for predicting mixing-layer noise
    • DOI 10.2514/1.22186
    • A. Samanta, J.B. Freund, M. Wei, S.K. Lele, Robustness of acoustic analogies for predicting mixing-layer noise, AIAA Journal 44 (11) (2006) 27802786. (Pubitemid 44788075)
    • (2006) AIAA Journal , vol.44 , Issue.11 , pp. 2780-2786
    • Samanta, A.1    Freund, J.B.2    Wei, M.3    Lele, S.K.4
  • 12
    • 0034321712 scopus 로고    scopus 로고
    • Numerical simulation of a Mach 1.92 turbulent jet and its sound field
    • J.B. Freund, S.K. Lele, and P. Moin Direct numerical simulation of a Mach 1.92 turbulent jet and its sound field AIAA Journal 38 11 2000 2023 2031 (Pubitemid 32021945)
    • (2000) AIAA journal , vol.38 , Issue.11 , pp. 2023-2031
    • Freund, J.B.1    Lele, S.K.2    Moin, P.3
  • 13
    • 0035838521 scopus 로고    scopus 로고
    • Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9
    • DOI 10.1017/S0022112001004414
    • J.B. Freund Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9 Journal of Fluid Mechanics 438 2001 277 305 (Pubitemid 32653257)
    • (2001) Journal of Fluid Mechanics , vol.438 , pp. 277-305
    • Freund, J.B.1
  • 14
    • 19944370497 scopus 로고    scopus 로고
    • Jet noise prediction of cold and hot subsonic jets using large-eddy simulation
    • D.J. Bodony, S.K. Lele, Jet noise prediction of cold and hot subsonic jets using large-eddy simulation, AIAA Paper 2004-3022, 2004.
    • (2004) AIAA Paper 2004-3022
    • Bodony, D.J.1    Lele, S.K.2
  • 15
    • 34347263398 scopus 로고    scopus 로고
    • Review of the current status of jet noise predictions using large-eddy simulation
    • D.J. Bodony, S.K. Lele, Review of the current status of jet noise predictions using large-eddy simulation, AIAsA Paper 2006-0468, 2006.
    • (2006) AIAsA Paper 2006-0468
    • Bodony, D.J.1    Lele, S.K.2
  • 16
    • 69949171616 scopus 로고    scopus 로고
    • Simulation of noise generation in the near-nozzle region of a chevron nozzle jet
    • A. Uzun, and M.Y. Hussaini Simulation of noise generation in the near-nozzle region of a chevron nozzle jet AIAA Journal 47 8 2009 1793 1810
    • (2009) AIAA Journal , vol.47 , Issue.8 , pp. 1793-1810
    • Uzun, A.1    Hussaini, M.Y.2
  • 17
    • 78649882346 scopus 로고    scopus 로고
    • Large-eddy simulations of perfectly-expanded supersonic jets: Quality assessment and validation
    • January 2010
    • S. Mende, M. Shoeybi, A. Sharma, F. Ham, S. Lele, P. Moin, Large-eddy simulations of perfectly-expanded supersonic jets: quality assessment and validation, AIAA Paper 2010-0271, January 2010.
    • AIAA Paper 2010-0271
    • Mende, S.1    Shoeybi, M.2    Sharma, A.3    Ham, F.4    Lele, S.5    Moin, P.6
  • 18
    • 64249092539 scopus 로고    scopus 로고
    • Simulation of a hot coaxial jet: Direct noise prediction and flow-acoustics correlations
    • C. Bogey, S. Barré, D. Juvé, and C. Bailly Simulation of a hot coaxial jet: direct noise prediction and flow-acoustics correlations Physics of Fluids 21 2009 035105
    • (2009) Physics of Fluids , vol.21 , pp. 035105
    • Bogey, C.1    Barré, S.2    Juvé, D.3    Bailly, C.4
  • 19
    • 84884742626 scopus 로고    scopus 로고
    • Identification of sound sources in large-eddy simulations of jets
    • May 2007
    • P. Spalart, M. Shur, M. Strelets, Identification of sound sources in large-eddy simulations of jets, AIAA Paper 2007-3616, May 2007.
    • AIAA Paper 2007-3616
    • Spalart, P.1    Shur, M.2    Strelets, M.3
  • 21
    • 76949091759 scopus 로고    scopus 로고
    • Extremizing feedback control of a high-speed and high Reynolds number jet
    • A. Sinha, K. Kim, J.-H. Kim, A. Serrani, and M. Samimy Extremizing feedback control of a high-speed and high Reynolds number jet AIAA Journal 48 2 2010 387 399
    • (2010) AIAA Journal , vol.48 , Issue.2 , pp. 387-399
    • Sinha, A.1    Kim, K.2    Kim, J.-H.3    Serrani, A.4    Samimy, M.5
  • 22
    • 0035335927 scopus 로고    scopus 로고
    • Evolution strategies for automatic optimization of jet mixing
    • P. Koumoutsakos, J.B. Freund, and D. Parekh Evolution strategies for automatic optimization of jet mixing AIAA Journal 39 5 2001 967 969 (Pubitemid 32471228)
    • (2001) AIAA Journal , vol.39 , Issue.5 , pp. 967-969
    • Koumoutsakos, P.1    Freund, J.2    Parekh, D.3
  • 24
    • 0035950842 scopus 로고    scopus 로고
    • DNS-based predictive control of turbulence: An optimal benchmark for feedback algorithms
    • T.R. Bewley, P. Moin, and R. Temam Dns-based predictive control of turbulence: an optimal benchmark target for feedback algorithms Journal of Fluid Mechanics 447 2001 179 225 (Pubitemid 33056279)
    • (2001) Journal of Fluid Mechanics , vol.447 , pp. 179-225
    • Bewley, T.R.1    Moin, P.2    Temam, R.3
  • 25
    • 31144458514 scopus 로고    scopus 로고
    • A noise-controlled free shear flow
    • DOI 10.1017/S0022112005007093, PII S0022112005007093
    • M. Wei, and J.B. Freund A noise-controlled free shear flow Journal of Fluid Mechanics 546 2006 123 152 (Pubitemid 43124742)
    • (2006) Journal of Fluid Mechanics , vol.546 , pp. 123-152
    • Wei, M.1    Freund, J.B.2
  • 26
    • 30744445022 scopus 로고    scopus 로고
    • PhD Thesis, Department of Theoretical and Applied Mechanics, University of Illinois at Urbana-Champaign, Urbana, Illinois
    • M. Wei, Jet Noise Control by Adjoint-based Optimization, PhD Thesis, Department of Theoretical and Applied Mechanics, University of Illinois at Urbana-Champaign, Urbana, Illinois, 2004.
    • (2004) Jet Noise Control by Adjoint-based Optimization
    • Wei, M.1
  • 28
    • 33845653135 scopus 로고    scopus 로고
    • Adjoint-based control of the noise from a turbulent mixing layer
    • May 2006
    • R.R. Kleinman, J.B. Freund, Adjoint-based control of the noise from a turbulent mixing layer, AIAA Paper 2006-2501, May 2006.
    • AIAA Paper 2006-2501
    • Kleinman, R.R.1    Freund, J.B.2
  • 29
    • 85088735797 scopus 로고    scopus 로고
    • Small changes that make a mixing layer very, very quiet
    • J.B. Freund, M. Wei, Small changes that make a mixing layer very, very quiet, AIAA Paper 2005-0997, 2005.
    • (2005) AIAA Paper 2005-0997
    • Freund, J.B.1    Wei, M.2
  • 30
    • 78149450777 scopus 로고    scopus 로고
    • Unsteady optimization using a discrete adjoint approach applied to aeroacoustic shape design
    • M.P. Rumpfkeil, D.W. Zingg, Unsteady optimization using a discrete adjoint approach applied to aeroacoustic shape design, AIAA Paper 2008-0018, 2008.
    • (2008) AIAA Paper 2008-0018
    • Rumpfkeil, M.P.1    Zingg, D.W.2
  • 31
    • 0016474762 scopus 로고
    • Basic principles of aerodynamic noise generation
    • D.G. Crighton Basic principles of aerodynamic noise generation Progress in Aerospace Sciences 16 1975 31 96
    • (1975) Progress in Aerospace Sciences , vol.16 , pp. 31-96
    • Crighton, D.G.1
  • 32
    • 0000977285 scopus 로고    scopus 로고
    • Proposed inflow/outflow boundary condition for direct computation of aerodynamic sound
    • J.B. Freund A proposed inflow/outflow boundary condition for direct computation of aerodynamic sound AIAA Journal 35 4 1997 740 742 (Pubitemid 127580087)
    • (1997) AIAA Journal , vol.35 , Issue.4 , pp. 740-742
    • Freund, J.B.1
  • 34
    • 77953216814 scopus 로고    scopus 로고
    • Active control of noise in supersonic jets using plasma actuators
    • Sea and Air GT2009 June 8-12, 2009, Orlando, Florida, gT2009-59456, June 2009
    • M. Samimy, J.H. Kim, M. Kearney-Fischer, Active control of noise in supersonic jets using plasma actuators, Proceedings of ASME Turbo Expo 2009: Power for Land, Sea and Air GT2009 June 812, 2009, Orlando, Florida, gT2009-59456, June 2009.
    • Proceedings of ASME Turbo Expo 2009: Power for Land
    • Samimy, M.1    Kim, J.H.2    Kearney-Fischer, M.3


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