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Volumn 122, Issue 3, 2000, Pages 442-449

Boundary layer transition induced by periodic wakes

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FRICTION; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; TURBOMACHINE BLADES; WAKES;

EID: 0034233129     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1303076     Document Type: Article
Times cited : (30)

References (18)
  • 7
    • 0025009655 scopus 로고
    • Compressor blade boundary layers, part 1: Test facility and measurements with no incident wakes; part 2: Measurements with incident wakes
    • (1990) ASME J. Turbomach. , vol.112 , pp. 222-240
    • Dong, Y.1    Cumpsty, N.A.2
  • 8
    • 0027681760 scopus 로고
    • Unsteady boundary layer transition in flow periodically disturbed by wakes
    • (1993) ASME J. Turbomach. , vol.115 , pp. 707-713
    • Orth, U.1
  • 10


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.