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Volumn 40, Issue 7, 2002, Pages 1363-1372

Active flow separation control on wall-mounted hump at high Reynolds numbers

Author keywords

[No Author keywords available]

Indexed keywords

ATTENUATION; BOUNDARY LAYER FLOW; CLOSED LOOP CONTROL SYSTEMS; CRYOGENICS; REYNOLDS NUMBER; TURBULENT FLOW; WALL FLOW;

EID: 0036642235     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1796     Document Type: Article
Times cited : (204)

References (26)
  • 16
    • 0005815144 scopus 로고
    • Fuselage self-propulsion by static-pressure thrust: Wind-tunnel verification
    • (1987) AIAA Paper , vol.87 , Issue.2935
    • Goldschmied, F.R.1
  • 18
  • 20
    • 0003247184 scopus 로고
    • Evolution, calibration, and operational characteristics of the two-dimensional test section of the langley 0.3-meter transonic cryogenic tunnel
    • (1987) NASA TP-2749
    • Ladson, C.A.1    Ray, E.J.2
  • 23
    • 3042776403 scopus 로고    scopus 로고
    • Active control of separated flows on generic configurations at high reynolds numbers (invited)
    • June
    • (1999) AIAA Paper , vol.99 , Issue.3403
    • Seifert, A.1    Pack, L.G.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.