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Volumn 17, Issue 4, 2007, Pages 263-272

Numerical prediction of supersonic jet screech frequency

Author keywords

Jet screech; Large Eddy simulation; Screech frequency; Standing wave

Indexed keywords


EID: 36448961249     PISSN: 09381287     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00193-007-0110-1     Document Type: Article
Times cited : (14)

References (23)
  • 1
    • 0001526919 scopus 로고
    • On the mechanism of choked jet noise
    • Powell A. (1953). On the mechanism of choked jet noise. Proc. Phys. Soc. Lond. 66: 1039-1056
    • (1953) Proc. Phys. Soc. Lond. , vol.66 , pp. 1039-1056
    • Powell, A.1
  • 2
    • 0001254490 scopus 로고
    • On the noise emanating from a two-dimensional jet above the critical pressure
    • Powell A. (1953). On the noise emanating from a two-dimensional jet above the critical pressure. Aeronaut. Q. 4: 103-122
    • (1953) Aeronaut. Q. , vol.4 , pp. 103-122
    • Powell, A.1
  • 3
    • 0001269929 scopus 로고    scopus 로고
    • Supersonic jet screech: Half-Century from Powell to present
    • Raman G. (1999). Supersonic jet screech: Half-Century from Powell to present. J. Sound Vib. 225: 543-571
    • (1999) J. Sound Vib. , vol.225 , pp. 543-571
    • Raman, G.1
  • 4
    • 0032074191 scopus 로고    scopus 로고
    • Shock oscillation in under expanded screeching jets
    • Panda J. (1998). Shock oscillation in under expanded screeching jets. J. Fluid Mech. 363: 81-116
    • (1998) J. Fluid Mech. , vol.363 , pp. 81-116
    • Panda, J.1
  • 5
    • 0032637214 scopus 로고    scopus 로고
    • An experimental investigation of screech noise generation
    • Panda J. (1999). An experimental investigation of screech noise generation. J. Fluid Mech. 378: 71-96
    • (1999) J. Fluid Mech. , vol.378 , pp. 71-96
    • Panda, J.1
  • 6
    • 0000381929 scopus 로고    scopus 로고
    • Measurement of shock structure and shock-vortex interaction in under-expanded jets using Rayleigh scattering
    • 12
    • Panda J. and Seasholtz R.G. (1999). Measurement of shock structure and shock-vortex interaction in under-expanded jets using Rayleigh scattering. Phys. Fluids 11(12): 3761-3777
    • (1999) Phys. Fluids , vol.11 , pp. 3761-3777
    • Panda, J.1    Seasholtz, R.G.2
  • 7
    • 85040296130 scopus 로고
    • Measurements of mean static pressure and far-field acoustic of shock-containing supersonic jets
    • Norum, T., Seiner J.: Measurements of mean static pressure and far-field acoustic of shock-containing supersonic jets. NASA TM 84521 (1982)
    • (1982) NASA TM , pp. 84521
    • Norum, T.1    Seiner, J.2
  • 8
    • 4244204220 scopus 로고    scopus 로고
    • Near field pressure fluctuations in the exit plane of a choked axisymmetric nozzle
    • Ponton, M.K., Seiner, J.M., Brown, M.C.: Near field pressure fluctuations in the exit plane of a choked axisymmetric nozzle. NASA TM 113137 (1997)
    • (1997) NASA TM , pp. 113137
    • Ponton, M.K.1    Seiner, J.M.2    Brown, M.C.3
  • 9
    • 0942279341 scopus 로고    scopus 로고
    • Time accurate numerical study of turbulent supersonic jets
    • Rona A. and Zhang X. (2004). Time accurate numerical study of turbulent supersonic jets. J. Sound Vib. 270: 297-321
    • (2004) J. Sound Vib. , vol.270 , pp. 297-321
    • Rona, A.1    Zhang, X.2
  • 10
    • 24144453171 scopus 로고    scopus 로고
    • Numerical simulation of the generation mechanism of axisymmetric supersonic jet screech tones
    • Li X.D. and Gao J.H. (2005). Numerical simulation of the generation mechanism of axisymmetric supersonic jet screech tones. Phys. Fluids 17: 085105-0851058
    • (2005) Phys. Fluids , vol.17 , pp. 085105-0851058
    • Li, X.D.1    Gao, J.H.2
  • 11
    • 0036151748 scopus 로고    scopus 로고
    • Three dimensional numerical simulation of the jet screech phenomenon
    • 1
    • Shen H. and Tam C.K.W. (2002). Three dimensional numerical simulation of the jet screech phenomenon. AIAA J. 40(1): 33-41
    • (2002) AIAA J. , vol.40 , pp. 33-41
    • Shen, H.1    Tam, C.K.W.2
  • 12
    • 0001957739 scopus 로고
    • General circulation experiments with the primitive equations, part I: The basic experiment
    • Smagorinsky J. (1963). General circulation experiments with the primitive equations, part I: the basic experiment. Mon. Weather Rev. 91: 99-152
    • (1963) Mon. Weather Rev. , vol.91 , pp. 99-152
    • Smagorinsky, J.1
  • 13
    • 0036640792 scopus 로고    scopus 로고
    • Large-Eddy Simulation of a Turbulent Compressible Round jet
    • 7
    • DeBonis J.R. and Scott J.N. (2002). Large-Eddy Simulation of a Turbulent Compressible Round jet. AIAA J. 40(7): 1346-1354
    • (2002) AIAA J. , vol.40 , pp. 1346-1354
    • Debonis, J.R.1    Scott, J.N.2
  • 15
    • 0001568854 scopus 로고
    • Efficient implementation of essentially non-oscillatory shock-capturing schemes, 2
    • Shu C.W. and Osher S. (1989). Efficient implementation of essentially non-oscillatory shock-capturing schemes, 2. J. Comp. Phys. 83: 32-78
    • (1989) J. Comp. Phys. , vol.83 , pp. 32-78
    • Shu, C.W.1    Osher, S.2
  • 16
    • 84896881532 scopus 로고    scopus 로고
    • Near field screech noise computation for an under-expanded supersonic jet by the CE/SE method
    • Loh, C.Y., Hultgren, L.S., Jorgenson P.C.E.: Near field screech noise computation for an under-expanded supersonic jet by the CE/SE method. AIAA paper 2001-2252 (2001)
    • (2001) AIAA Paper , pp. 2001-2252
    • Loh, C.Y.1    Hultgren, L.S.2    Jorgenson, P.C.E.3
  • 17
    • 0002942882 scopus 로고
    • The effects of nozzle exit lip thickness on plume resonance
    • Ponton M.K. and Seiner J.M. (1992). The effects of nozzle exit lip thickness on plume resonance. J. Sound Vib. 154: 531-549
    • (1992) J. Sound Vib. , vol.154 , pp. 531-549
    • Ponton, M.K.1    Seiner, J.M.2
  • 18
    • 84896694169 scopus 로고    scopus 로고
    • Computing axisymmetric jet screech tones using unstructured grids
    • Jorgenson, P.C.E., Loh, C.Y.: Computing axisymmetric jet screech tones using unstructured grids. AIAA paper 2002-3889 (2002)
    • (2002) AIAA Paper , pp. 2002-3889
    • Jorgenson, P.C.E.1    Loh, C.Y.2
  • 19
    • 0006098223 scopus 로고
    • A note on Prandtl's formula for the wavelength of a supersonic gas jet
    • Pack D. (1950). A note on Prandtl's formula for the wavelength of a supersonic gas jet. Q. J. Mech. Appl. Math. III: 173-181
    • (1950) Q. J. Mech. Appl. Math. , vol.3 , pp. 173-181
    • Pack, D.1
  • 20
    • 84977091131 scopus 로고    scopus 로고
    • Under-expanded screeching jets from circular, rectangular and elliptic nozzles
    • Panda, J., Raman, G., Zaman, K.B.M.Q.: Under-expanded screeching jets from circular, rectangular and elliptic nozzles. AIAA Paper 97-1623 (1997)
    • (1997) AIAA Paper , pp. 97-1623
    • Panda, J.1    Raman, G.2    Zaman, K.B.M.Q.3
  • 21
    • 85003263016 scopus 로고
    • The preferred mode of instability for a Mach 2 jet
    • Seiner, J., Manning, J., Ponton, M.: The preferred mode of instability for a Mach 2 jet. AIAA Paper 86-1942 (1986)
    • (1986) AIAA Paper , pp. 86-1942
    • Seiner, J.1    Manning, J.2    Ponton, M.3
  • 22
    • 0006091338 scopus 로고
    • Aerodynamic aspects of shocks containing jet plumes
    • Seiner, J., Norum, T., Manning, J.: Aerodynamic aspects of shocks containing jet plumes. AIAA Paper 80-0965 (1980)
    • (1980) AIAA Paper , pp. 80-0965
    • Seiner, J.1    Norum, T.2    Manning, J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.