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Volumn 40, Issue 6, 2002, Pages 1164-1169

Large-scale structures and growth of a flat plate compressible wake

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPRESSIBLE FLOW; REYNOLDS NUMBER; WIND TUNNELS;

EID: 0036603195     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1767     Document Type: Article
Times cited : (14)

References (35)
  • 14
    • 0025463399 scopus 로고
    • Experimental investigation of vortex formation in the wake of a flat plate for subsonic and supersonic freestream mach numbers
    • (1990) Experiments in Fluids , vol.9 , Issue.9 , pp. 267-272
    • Althaus, W.1
  • 25
    • 0016510313 scopus 로고
    • Investigation of supersonic turbulent mixing layer with zero pressure gradient
    • (1975) AIAA Journal , vol.13 , Issue.5 , pp. 566-572
    • Ikawa, H.1    Kubota, T.2
  • 27
    • 0005949707 scopus 로고
    • Measurement of the recovery temperature in the wake of a cylinder and of a wedge at mach numbers between 0.5 and 3
    • FFA, Aeronautical Research Inst. of Sweden, Rept. 84, Stockholm
    • (1959)
    • Thomann, H.1
  • 30
    • 0015064017 scopus 로고
    • Experimental stability studies in wakes of two-dimensional slender bodies at hypersonic speeds
    • (1971) AIAA Journal , vol.9 , Issue.5 , pp. 851-857
    • Behrens, W.1    Ko, D.R.S.2
  • 35
    • 84963758363 scopus 로고    scopus 로고
    • Compressibility effects on entrainment and mixing in supersonic planar turbulent wakes
    • AIAA Paper 99-3582, June/July
    • (1999)
    • Nakagawa, M.1    Dahm, W.J.A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.