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Volumn 30, Issue 2, 2001, Pages 221-228

Experimental study of the unsteady aerodynamic field outside a tunnel during a train entry

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE PROPAGATION; AERODYNAMICS; ATMOSPHERIC PRESSURE; BOUNDARY CONDITIONS; COMPRESSIBLE FLOW; FLOW VISUALIZATION; METHOD OF MOMENTS; PRESSURE EFFECTS; PRESSURE MEASUREMENT; REYNOLDS NUMBER; TRAIN FERRIES; VELOCITY MEASUREMENT; VORTEX FLOW;

EID: 0035243213     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s003480000159     Document Type: Article
Times cited : (43)

References (18)
  • 7
    • 0001952348 scopus 로고    scopus 로고
    • Mach number dependence of the compression wave generated by a high-speed train entering a tunnel
    • (1998) J Sound Vib , vol.212 , pp. 23-36
    • Howe, M.S.1
  • 8
    • 0002834275 scopus 로고
    • Numerical simulation of compression wave in tunnels during train nose entry (in Japanese)
    • (1994) Railway Tech Res Inst Rep , vol.8 , Issue.6 , pp. 25-30
    • Iida, M.1
  • 15
    • 0018026770 scopus 로고
    • The large-scale structure of unsteady self-similar rolled-up vortex sheets
    • (1978) J Fluid Mech , vol.88 , pp. 401-430
    • Pullin, D.I.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.