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NTIS 바로가기한국항공우주학회지 = Journal of the Korean Society for Aeronautical & Space Sciences, v.38 no.8, 2010년, pp.790 - 797
Mode transition of the axi-symmetric screech tone in the low supersonic Mach number range from 1.0 to 1.20 is numerically analyzed. The axi-symmetric Navier-Stokes equations and the k-e turbulence model are solved in the cylindrical coordinate system. The dispersion-relation-preserving(DRP) scheme i...
A. Powell, "On the Mechanism of Choked Jet Noise", Proceedings of the Physical Society, London, Vol. 66, 1953, pp. 1039-1056.
R. Westley, and J. H. Woolley, "An Investigation of the Near Noise Fields of a Choked Axisymmetric Jet", Proceedings of AFOSR-V, Ribner, pp. 147-167.
M. Harper-Bourne, and M. J. Fisher, "The Noise from Shock Waves in Supersonic Jets", AGARD CP131, Noise Mechanism, 1974.
C. K. W. Tam, "Proposed Relationship Between Broadband Shock Associated Noise and Screech Tones", Journal of Sound and Vibration, Vol. 110, 1986, pp. 309-321.
K. C. Massey, and K. K. Ahuja, "Screech Frequency Prediction in Light of Mode Detection and Convection Speed Measurements for Heated Jets", AIAA paper 97-1625, 1997.
J. Panda, "Shock Oscillation in Underexpanded Screeching Jets", Journal of Fluid and Mechanics, Vol. 363, 1998, pp. 173-198.
G. Raman, "Supersonic Jet Screech: Half-Century from Powell to the Present", Journal of Sound and Vibration, Vol. 225, No. 3, 1999, pp. 543-571.
A. T. Thies, and C. K. W. Tam, "Computation of Turbulent Axisymmetric and Nonaxisymmetric Jet Flows Using the k-e Model", AIAA Journal, Vol. 34, No. 2, 1996, pp. 309-316.
C. K. W. Tam, "Computational Aeroacoustics: Issues and Methods", AIAA Journal, Vol. 33, No. 10, 1995, pp. 1788-1796.
H. Shen, and C. K. W. Tam, "Numerical Simulation of the Generation of Axisymmetric Mode Jet Screech Tones", AIAA Journal, Vol. 36, No. 10, 1998, pp. 1801-1807.
J. Bin, M. Kim, S. Lee, "A numerical study on the generation of impulsive noise by complex flows discharging from a muzzle", International Journal for Numerical Methods in Engineering, Vol. 75, 2008, pp. 964-991.
C. K. W. Tam and Z. Dong, "Wall Boundary Conditions for High-Order Finite Difference Schemes in Computational Aeroacoustics", Theoretical and Computational Fluid Dynamics, Vol. 8, 1994, pp. 303-322.
T. Colonius, "Modeling Artificial Boundary Conditions for Compressible Flow",
C. K. W. Tam, and K. A. Kurbatskii, "Multi-Size-Mesh Multi-Time-Step Dispersion-Relation-Preserving Scheme for Multiple-Scale Aeroacoustics Problems", International Journal of Computational Fluid Dynamics, Vol. 17, 2003, pp. 119-132.
T. D. Norum, and M. C. Brown, "Simulated High-speed Flight Effects on Supersonic Jet Noise", AIAA Paper No. 1993-4388, 1993.
M. K. Ponton, and J. M. Seiner, "The Effects of Nozzle Exit Lip Thickness on Plume Resonance", Journal of Sound and Vibration, Vol. 154, No. 3, 1992, pp. 531-549.
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