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Volumn 318, Issue SECTION 3, 2011, Pages

Large-eddy simulation of subsonic jets

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; DIRECT INJECTION; FIGHTER AIRCRAFT; INCOMPRESSIBLE FLOW; MIXING; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; RUNGE KUTTA METHODS; SUBSONIC AERODYNAMICS; TURBULENCE;

EID: 84863054233     PISSN: 17426588     EISSN: 17426596     Source Type: Conference Proceeding    
DOI: 10.1088/1742-6596/318/3/032052     Document Type: Conference Paper
Times cited : (17)

References (10)
  • 1
    • 84982318676 scopus 로고    scopus 로고
    • Large-eddy simulation of a Mach 0.9 turbulent jet
    • BOERSMA, B. J. & LELE, S. K., Large-eddy simulation of a Mach 0.9 turbulent jet, AIAA Journal, 99, (1999).
    • (1999) AIAA Journal , vol.99
    • Boersma, B.J.1    Lele, S.K.2
  • 2
    • 0037360678 scopus 로고    scopus 로고
    • Noise investigation of a high subsonic, moderate Reynolds number jet using a compressible large-eddy simulation
    • BOGEY, C., BAILLY, C. & JUVÉ, D., Noise investigation of a high subsonic, moderate Reynolds number jet using a compressible large-eddy simulation, Theoret.Comput.Fluid Dynamics, 16, 273-297, (2003).
    • (2003) Theoret.Comput.Fluid Dynamics , vol.16 , pp. 273-297
    • Bogey, C.1    Bailly, C.2    Juvé, D.3
  • 3
    • 9944264070 scopus 로고    scopus 로고
    • Computational aeroacoustics: Progress on nonlinear problems of sound generation
    • COLONIUS, T. & LELE, S. K., Computational aeroacoustics: progress on nonlinear problems of sound generation, Progress in Aerospace Sciences, 40, 345-416, (2004).
    • (2004) Progress in Aerospace Sciences , vol.40 , pp. 345-416
    • Colonius, T.1    Lele, S.K.2
  • 5
    • 0000977285 scopus 로고    scopus 로고
    • Proposed in ow/out flow boundary condition for direct computation of aerodynamic sound
    • FREUND, J. B., Proposed in ow/out flow boundary condition for direct computation of aerodynamic sound, AIAA Journal, 35, 4, (1997).
    • (1997) AIAA Journal , vol.35 , pp. 4
    • Freund, J.B.1
  • 6
    • 49049143188 scopus 로고
    • High-Re solutions for incompressible flow using the Navier-Stokes equations and the multigrid method
    • GHIA, U., High-Re solutions for incompressible flow using the Navier-Stokes equations and the multigrid method, J.Comput.Phys. 48, 3, 387-411, (1982).
    • (1982) J.Comput.Phys. , vol.48 , Issue.3 , pp. 387-411
    • Ghia, U.1
  • 7
    • 84863035916 scopus 로고    scopus 로고
    • Doctoral Thesis, Delft University of Technology, ISBN-978-90-9024705-2
    • MOORE, P. D., Aeroacoustics of compressible subsonic jets, Doctoral Thesis, Delft University of Technology, ISBN-978-90-9024705-2, (2009).
    • (2009) Aeroacoustics of Compressible Subsonic Jets
    • Moore, P.D.1
  • 9
    • 76749084752 scopus 로고    scopus 로고
    • Density and compressibility effects in turbulent subsonic jets part 1: Mean velocity field
    • WANG, Z. & ANDREOPOULOS, Y., Density and compressibility effects in turbulent subsonic jets part 1: mean velocity field, Exp. Fluids, 48, 327-343, (2010).
    • (2010) Exp. Fluids , vol.48 , pp. 327-343
    • Wang, Z.1    Andreopoulos, Y.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.