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Volumn 330, Issue 8, 2002, Pages 527-533

Downstream subsonic jet noise: Link with vortical structures intruding into the jet core

Author keywords

Acoustics; Computational aeroacoustics; Jet noise; Large Eddy Simulation

Indexed keywords

ACOUSTICS; FLUID FLOW; JET FLOW; LARGE EDDY SIMULATION; SUBSONIC FLOW; VORTICITY;

EID: 0036690924     PISSN: 16310721     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1631-0721(02)01499-7     Document Type: Article
Times cited : (5)

References (13)
  • 1
    • 0029380030 scopus 로고
    • Computational aeroacoustics: Issues and methods
    • (1995) AIAA J. , vol.33 , Issue.10 , pp. 1788-1796
    • Tam, C.K.W.1
  • 2
  • 4
    • 0000365708 scopus 로고    scopus 로고
    • Numerical simulation of the generation of the axisymmetric mode jet screech tones
    • (1998) AIAA J. , vol.36 , Issue.10 , pp. 1801-1807
    • Shen, H.1    Tam, C.K.W.2
  • 6
    • 14244272449 scopus 로고    scopus 로고
    • Three-dimensional non-reflective boundary conditions for acoustic simulations: Far field formulation and validation test cases
    • to appear
    • (2002) Acustica
    • Bogey, C.1    Bailly, C.2
  • 12
    • 84896838364 scopus 로고
    • Measurements of subsonic jet noise and comparison with theory
    • (1971) J. Fluid Mech. , vol.46 , Issue.3 , pp. 477-500
    • Lush, P.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.