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Volumn 224, Issue 1, 2007, Pages 449-463

Simulation and measurement of flow generated noise

Author keywords

Compressible flow; Computation; Direct numerical Simulation; FFowcs Williams Hawkings method; Jet flow; Low Reynolds number; Navier Stokes equations; Numerical methods; Subsonic

Indexed keywords

ACOUSTIC FIELD MEASUREMENT; ACOUSTIC FIELDS; DIRECT NUMERICAL SIMULATION; NAVIER STOKES EQUATIONS; NUMERICAL MODELS; REYNOLDS NUMBER;

EID: 34248232011     PISSN: 00219991     EISSN: 10902716     Source Type: Journal    
DOI: 10.1016/j.jcp.2007.04.006     Document Type: Article
Times cited : (14)

References (13)
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    • Crighton, D.1
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    • J.B. Freund, Direct numerical simulation of the noise from a Mach 0.9 jet, ASME FEDSM 99-7251, 1999.
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    • Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9
    • Freund J.B. Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9. J. Fluid Mech. 438 (2001) 277-305
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    • Freund, J.B.1
  • 9
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    • On sound generated aerodynamically, part 1: General theory
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.