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Volumn 20, Issue 3, 2008, Pages

Numerical simulation of the three-dimensional screech phenomenon from a circular jet

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FLOW FIELDS; MACH NUMBER; NAVIER STOKES EQUATIONS; NOZZLES; RUNGE KUTTA METHODS;

EID: 41849133538     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.2844474     Document Type: Article
Times cited : (45)

References (34)
  • 1
    • 0001254490 scopus 로고
    • "On the noise emanating from a two-dimensional jet above the critical pressure"
    • AEQUAY0001-9259
    • A. Powell, "On the noise emanating from a two-dimensional jet above the critical pressure," Aeronaut. Q. AEQUAY0001-9259 4, 103 (1953).
    • (1953) Aeronaut. Q. , vol.4 , pp. 103
    • Powell, A.1
  • 2
    • 0001269929 scopus 로고    scopus 로고
    • "Supersonic jet screech: Half-century from Powell to the present"
    • JSVIAG0022-460X10.1006/jsvi.1999.2181
    • G. Raman, "Supersonic jet screech: Half-century from Powell to the present," J. Sound Vib. JSVIAG0022-460X10.1006/jsvi.1999.2181 225, 543 (1999).
    • (1999) J. Sound Vib. , vol.225 , pp. 543
    • Raman, G.1
  • 3
    • 0038929560 scopus 로고
    • "Sur la fréquencies des ondes émises par un jet d'air á grande vitesse"
    • COREAF0001-4036
    • M. Merle, "Sur la fréquencies des ondes émises par un jet d'air á grande vitesse," Acad. Sci., Paris, C. R. COREAF0001-4036 243, 490 (1956).
    • (1956) Acad. Sci., Paris, C. R. , vol.243 , pp. 490
    • Merle, M.1
  • 4
    • 0039134881 scopus 로고
    • "Tones from a choked axisymmetric jet"
    • ACUSAY0001-7884
    • M. G. Davies and D. E. S. Oldfield, "Tones from a choked axisymmetric jet," Acustica ACUSAY0001-7884 12, 257 (1962).
    • (1962) Acustica , vol.12 , pp. 257
    • Davies, M.G.1    Oldfield, D.E.S.2
  • 5
    • 0008081178 scopus 로고
    • "An investigation of the near noise field of a choked axisymmetric air jet"
    • National Aeronautical Establishment (Canada) Aero. Report LR 506, June
    • R. Westley and J. H. Woolley, "An investigation of the near noise field of a choked axisymmetric air jet," National Aeronautical Establishment (Canada) Aero. Report LR 506, June, 1968.
    • (1968)
    • Westley, R.1    Woolley, J.H.2
  • 6
    • 0038929559 scopus 로고
    • "Aerosonic games with the aid of control elements and externally generated pulses"
    • AGCPAV0549-7191, 20.1
    • L. J. Poldervaart, A. P. Wijnands, and L. Bronkhurst, "Aerosonic games with the aid of control elements and externally generated pulses," AGARD Conf. Proc. AGCPAV0549-7191 CP-131, 20.1 (1973).
    • (1973) AGARD Conf. Proc. , vol.CP-131
    • Poldervaart, L.J.1    Wijnands, A.P.2    Bronkhurst, L.3
  • 7
    • 85042206967 scopus 로고    scopus 로고
    • "A simple model of shock cell noise generation and its reduction"
    • National Aeronautical Establishment (Canada) Aero. Report LR 564, 1972
    • Y. Y. Chan, "A simple model of shock cell noise generation and its reduction," National Aeronautical Establishment (Canada) Aero. Report LR 564, 1972.
    • Chan, Y.Y.1
  • 8
    • 0002942882 scopus 로고
    • "The effects of nozzle exit lip thickness on plume resonance"
    • JSVIAG0022-460X10.1016/0022-460X(92)90784-U
    • M. K. Ponton and J. M. Seiner, "The effects of nozzle exit lip thickness on plume resonance," J. Sound Vib. JSVIAG0022-460X10.1016/ 0022-460X(92)90784-U 154, 531 (1992).
    • (1992) J. Sound Vib. , vol.154 , pp. 531
    • Ponton, M.K.1    Seiner, J.M.2
  • 9
    • 0032074191 scopus 로고    scopus 로고
    • "Shock oscillation in underexpanded screeching jets"
    • JFLSA70022-112010.1017/S0022112098008842
    • J. Panda, "Shock oscillation in underexpanded screeching jets," J. Fluid Mech. JFLSA70022-112010.1017/S0022112098008842 363, 173 (1998).
    • (1998) J. Fluid Mech. , vol.363 , pp. 173
    • Panda, J.1
  • 10
    • 0000381929 scopus 로고    scopus 로고
    • "Measurement of shock structure and shock-vortex interaction in underexpanded jets using Rayleigh scattering"
    • PHFLE61070-663110.1063/1.870247
    • J. Panda and R. G. Seasholtz, "Measurement of shock structure and shock-vortex interaction in underexpanded jets using Rayleigh scattering," Phys. Fluids PHFLE61070-663110.1063/1.870247 11, 3761 (1999).
    • (1999) Phys. Fluids , vol.11 , pp. 3761
    • Panda, J.1    Seasholtz, R.G.2
  • 11
    • 0022042964 scopus 로고
    • "A multiple-scales model of shock-cell structure of imperfectly expanded supersonic jets"
    • JFLSA70022-112010.1017/S0022112085001173
    • C. K. W. Tam, J. A. Jackson, and J. M. Seiner, "A multiple-scales model of shock-cell structure of imperfectly expanded supersonic jets," J. Fluid Mech. JFLSA70022-112010.1017/S0022112085001173 153, 123 (1985).
    • (1985) J. Fluid Mech. , vol.153 , pp. 123
    • Tam, C.K.W.1    Jackson, J.A.2    Seiner, J.M.3
  • 12
    • 0024701990 scopus 로고
    • "A linear shock-cell model for jets of arbitrary exit geometry"
    • JSVIAG0022-460X10.1016/0022-460X(89)90592-0
    • P. J. Morris, T. R. S. Bhat, and G. Chen, "A linear shock-cell model for jets of arbitrary exit geometry," J. Sound Vib. JSVIAG0022-460X10.1016/0022-460X(89)90592-0 132, 199 (1989).
    • (1989) J. Sound Vib. , vol.132 , pp. 199
    • Morris, P.J.1    Bhat, T.R.S.2    Chen, G.3
  • 13
    • 0022794738 scopus 로고
    • "Proposed relationship between broadband shock associated noise and screech tones"
    • JSVIAG0022-460X10.1016/S0022-460X(86)80212-7
    • C. K. W. Tam, J. M. Seiner, and J. C. Yu, "Proposed relationship between broadband shock associated noise and screech tones," J. Sound Vib. JSVIAG0022-460X10.1016/S0022-460X(86)80212-7 110, 309 (1986).
    • (1986) J. Sound Vib. , vol.110 , pp. 309
    • Tam, C.K.W.1    Seiner, J.M.2    Yu, J.C.3
  • 14
    • 0000365708 scopus 로고    scopus 로고
    • "Numerical simulation of the generation of axisymmetric mode jet screech tones"
    • AIAJAH0001-1452
    • H. Shen and C. K. W. Tam, "Numerical simulation of the generation of axisymmetric mode jet screech tones," AIAA J. AIAJAH0001-1452 36, 1801 (1998).
    • (1998) AIAA J. , vol.36 , pp. 1801
    • Shen, H.1    Tam, C.K.W.2
  • 15
    • 0036151748 scopus 로고    scopus 로고
    • "Three-dimensional numerical simulation of the jet screech phenomenon"
    • AIAJAH0001-1452
    • H. Shen and C. K. W. Tam, "Three-dimensional numerical simulation of the jet screech phenomenon," AIAA J. AIAJAH0001-1452 40, 33 (2002).
    • (2002) AIAA J. , vol.40 , pp. 33
    • Shen, H.1    Tam, C.K.W.2
  • 16
    • 24144453171 scopus 로고    scopus 로고
    • "Numerical simulation of the generation mechanism of axisymmetric supersonic jet screech tones"
    • PHFLE61070-663110.1063/1.2033909
    • X. D. Li and J. H. Gao, "Numerical simulation of the generation mechanism of axisymmetric supersonic jet screech tones," Phys. Fluids PHFLE61070-663110.1063/1.2033909 17, 085105 (2005).
    • (2005) Phys. Fluids , vol.17 , pp. 085105
    • Li, X.D.1    Gao, J.H.2
  • 17
    • 29244461004 scopus 로고    scopus 로고
    • "Numerical simulation of three-dimensional supersonic jet screech tones"
    • AIAA Pap. No. 2005-2882
    • X. D. Li and J. H. Gao, "Numerical simulation of three-dimensional supersonic jet screech tones," AIAA Pap. No. 2005-2882, 2005.
    • (2005)
    • Li, X.D.1    Gao, J.H.2
  • 18
    • 33845618548 scopus 로고    scopus 로고
    • "A numerical study of nozzle boundary layer thickness on axisymmetric supersonic jet screech tones"
    • AIAA Pap. No. 2006-2675
    • J. H. Gao and X. D. Li, "A numerical study of nozzle boundary layer thickness on axisymmetric supersonic jet screech tones," AIAA Pap. No. 2006-2675, 2006.
    • (2006)
    • Gao, J.H.1    Li, X.D.2
  • 19
    • 0003942284 scopus 로고    scopus 로고
    • "Near field screech noise computation for an underexpanded supersonic jet by the CE/SE method"
    • AIAA Pap. No. 2001-2252
    • C. Y. Loh, L. S. Hultgren, and P. C.E. Jorgenson, "Near field screech noise computation for an underexpanded supersonic jet by the CE/ SE method," AIAA Pap. No. 2001-2252, 2001.
    • (2001)
    • Loh, C.Y.1    Hultgren, L.S.2    Jorgenson, P.C.E.3
  • 20
    • 84896884165 scopus 로고    scopus 로고
    • "Computation of shock induced noise in imperfectly expanded supersonic jets"
    • AIAA Pap. No. 2002-2527
    • B. Imamoglu and P. Balakumar, "Computation of shock induced noise in imperfectly expanded supersonic jets," AIAA Pap. No. 2002-2527, 2002.
    • (2002)
    • Imamoglu, B.1    Balakumar, P.2
  • 21
    • 84894543035 scopus 로고    scopus 로고
    • "A 3-D CE/SE Navier-Stokes solver with unstructured hexahedral grid for computation of nearfield jet screech noise"
    • AIAA Pap. No. 2003-3207
    • C. Y. Loh, A. Himansu, and L. S. Hultgrent, "A 3-D CE/SE Navier-Stokes solver with unstructured hexahedral grid for computation of nearfield jet screech noise," AIAA Pap. No. 2003-3207, 2003.
    • (2003)
    • Loh, C.Y.1    Himansu, A.2    Hultgrent, L.S.3
  • 22
    • 84894594159 scopus 로고    scopus 로고
    • "Three dimensional computation of shock induced noise in imperfectly expanded supersonic jets"
    • AIAA Pap. No. 2003-3249
    • B. Imamoglu and P. Balakumar, "Three dimensional computation of shock induced noise in imperfectly expanded supersonic jets," AIAA Pap. No. 2003-3249, 2003.
    • (2003)
    • Imamoglu, B.1    Balakumar, P.2
  • 23
    • 34547815542 scopus 로고    scopus 로고
    • "Numerical study of screech generation in a planar supersonic jet"
    • PHFLE61070-663110.1063/1.2747225
    • J. Berland, C. Bogey, and C. Bailly, "Numerical study of screech generation in a planar supersonic jet," Phys. Fluids PHFLE61070-663110.1063/1.2747225 19, 075105 (2007).
    • (2007) Phys. Fluids , vol.19 , pp. 075105
    • Berland, J.1    Bogey, C.2    Bailly, C.3
  • 24
    • 85088748572 scopus 로고    scopus 로고
    • "Numerical simulation of shock-vortex interactions in supersonic jet screech"
    • AIAA Pap. No. 1998-0282
    • T. A. Manning and S. K. Lele, "Numerical simulation of shock-vortex interactions in supersonic jet screech," AIAA Pap. No. 1998-0282, 1998.
    • (1998)
    • Manning, T.A.1    Lele, S.K.2
  • 25
    • 84861291518 scopus 로고    scopus 로고
    • "Validation of a two-equation turbulence model for axisymmetric reacting and non-reaction flows"
    • AIAA Pap. No. 2000-3463
    • G. Turpin and J. Troyes, "Validation of a two-equation turbulence model for axisymmetric reacting and non-reaction flows," AIAA Pap. No. 2000-3463, 2000.
    • (2000)
    • Turpin, G.1    Troyes, J.2
  • 26
    • 19644369292 scopus 로고
    • "Dispersion-relation-preserving finite difference schemes for computational acoustics"
    • JCTPAH0021-999110.1006/jcph.1993.1142
    • C. K. W. Tam and J. C. Webb, "Dispersion-relation-preserving finite difference schemes for computational acoustics," J. Comput. Phys. JCTPAH0021-999110.1006/jcph.1993.1142 107, 262 (1993).
    • (1993) J. Comput. Phys. , vol.107 , pp. 262
    • Tam, C.K.W.1    Webb, J.C.2
  • 27
    • 0039496334 scopus 로고    scopus 로고
    • "2N-storage low-dissipation and low-dispersion Runge-Kutta schemes for computational aeroacoustics"
    • JCTPAH0021-999110.1006/jcph.1998.5986
    • D. Stanescu and W. G. Habashi, "2N-storage low-dissipation and low-dispersion Runge-Kutta schemes for computational aeroacoustics," J. Comput. Phys. JCTPAH0021-999110.1006/ jcph.1998.5986 143, 674 (1998).
    • (1998) J. Comput. Phys. , vol.143 , pp. 674
    • Stanescu, D.1    Habashi, W.G.2
  • 28
    • 4244204220 scopus 로고    scopus 로고
    • "Near field pressure fluctuations in the exit plane of a choked axisymmetric nozzle"
    • TM-113137
    • M. K. Ponton, J. M. Seiner, and M. C. Brown, "Near field pressure fluctuations in the exit plane of a choked axisymmetric nozzle," NASA Tech. Memo. TM-113137, 1997.
    • (1997) NASA Tech. Memo.
    • Ponton, M.K.1    Seiner, J.M.2    Brown, M.C.3
  • 29
    • 0344006664 scopus 로고    scopus 로고
    • "Low-dissipation and low-dispersion Runge-Kutta schemes for computational acoustics"
    • JCTPAH0021-999110.1006/jcph.1996.0052
    • F. Q. Hu, M. Y. Hussaini, and J. L. Manthey, "Low-dissipation and low-dispersion Runge-Kutta schemes for computational acoustics," J. Comput. Phys. JCTPAH0021-999110.1006/jcph.1996.0052 124, 177 (1996).
    • (1996) J. Comput. Phys. , vol.124 , pp. 177
    • Hu, F.Q.1    Hussaini, M.Y.2    Manthey, J.L.3
  • 30
    • 0008077577 scopus 로고
    • "Direct computation of nonlinear acoustic pulses using high order finite difference schemes"
    • AIAA Pap. No. 1993-4325
    • C. K.W. Tam and H. Shen, "Direct computation of nonlinear acoustic pulses using high order finite difference schemes," AIAA Pap. No. 1993-4325, 1993.
    • (1993)
    • Tam, C.K.W.1    Shen, H.2
  • 31
    • 14244272449 scopus 로고    scopus 로고
    • "Three-dimensional non-reflective boundary conditions for acoustic simulations: Far field formulation and validation test cases"
    • AAACDB1610-1928
    • C. Bogey and C. Bailly, "Three-dimensional non-reflective boundary conditions for acoustic simulations: Far field formulation and validation test cases," Acta. Acust. Acust. AAACDB1610-1928, 88, 463 (2002).
    • (2002) Acta. Acust. Acust. , vol.88 , pp. 463
    • Bogey, C.1    Bailly, C.2
  • 32
    • 0030518618 scopus 로고    scopus 로고
    • "Radiation and outflow boundary conditions for direct computation of acoustic and flow disturbances in a nonuniform mean flow"
    • JCOAEJ0218-396X10.1142/S0218396X96000040
    • C. K. W. Tam and Z. Dong, "Radiation and outflow boundary conditions for direct computation of acoustic and flow disturbances in a nonuniform mean flow," J. Comput. Acoust. JCOAEJ0218-396X10.1142/ S0218396X96000040 4, 175 (1996).
    • (1996) J. Comput. Acoust. , vol.4 , pp. 175
    • Tam, C.K.W.1    Dong, Z.2
  • 33
    • 0019548720 scopus 로고
    • "Effects of exit Mach number and temperature on mean-flow and turbulence characteristics in round jets"
    • JFLSA70022-112010.1017/S0022112081003170
    • J. C. Lau, "Effects of exit Mach number and temperature on mean-flow and turbulence characteristics in round jets," J. Fluid Mech. JFLSA70022-112010.1017/S0022112081003170 105, 193 (1981).
    • (1981) J. Fluid Mech. , vol.105 , pp. 193
    • Lau, J.C.1
  • 34
    • 0029256999 scopus 로고
    • "Acoustic study of B helical mode for choked axisymmetric nozzle"
    • AIAJAH0001-1452
    • M. K. Ponton and J. M. Seiner, "Acoustic study of B helical mode for choked axisymmetric nozzle," AIAA J.AIAJAH0001-1452 33, 413 (1995).
    • (1995) AIAA J. , vol.33 , pp. 413
    • Ponton, M.K.1    Seiner, J.M.2


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