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Volumn 52, Issue 2, 2012, Pages 511-517

On the stabilization of leading-edge vortices with spanwise flow

Author keywords

[No Author keywords available]

Indexed keywords

DIRECT FORCE MEASUREMENTS; LEADING-EDGE VORTICES; PARTICLE IMAGE VELOCIMETRIES; RELATIVE TIME; ROTATIONAL ACCELERATION; SPANWISE FLOW; SWEEPBACK ANGLE; TIP VORTEX;

EID: 84861795394     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00348-011-1241-9     Document Type: Article
Times cited : (54)

References (13)
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  • 2
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    • Vortex wake and flight kinematics of a swift in cruising flight in a wind tunnel
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    • Henningsson, P.1    Spedding, G.R.2    Hedenstrom, A.3
  • 5
    • 79959498445 scopus 로고    scopus 로고
    • Reynolds number effects on leading-edge vortex development on a waving wing
    • doi:10.1007/s00348-010-1037-3
    • Jones AR, Babinsky H (2011) Reynolds number effects on leading-edge vortex development on a waving wing. Exp Fluids 51(1):197-210. doi:10.1007/s00348-010-1037-3
    • (2011) Exp Fluids , vol.51 , Issue.1 , pp. 197-210
    • Jones, A.R.1    Babinsky, H.2
  • 6
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    • Experimental study of three-dimensional vortex structures in translating and rotating plates
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    • Kim, D.1    Gharib, M.2
  • 7
    • 68249108331 scopus 로고    scopus 로고
    • Rotational accelerations stabilize leading edge vortices on revolving fly wings
    • Lentink D, Dickinson MH (2009) Rotational accelerations stabilize leading edge vortices on revolving fly wings. J Exp Biol 212:2705-2719
    • (2009) J Exp Biol , vol.212 , pp. 2705-2719
    • Lentink, D.1    Dickinson, M.H.2
  • 9
    • 33846080021 scopus 로고    scopus 로고
    • Morphology of the forced oscillatory flow past a finite-span wing at low Reynolds number
    • Parker K, von Ellenrieder KD, Soria J (2007) Morphology of the forced oscillatory flow past a finite-span wing at low Reynolds number. J Fluid Mech 571:327-357
    • (2007) J Fluid Mech , vol.571 , pp. 327-357
    • Parker, K.1    Von Ellenrieder, K.D.2    Soria, J.3
  • 10
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    • Predictions of vortex-lift characteristics by a leading-edge suction analogy
    • Polhamus EC (1971) Predictions of vortex-lift characteristics by a leading-edge suction analogy. J Aircraft 8:193-199
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  • 11
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    • Shallow and deep dynamic stall for flapping low Reynolds number airfoils
    • Ol MV, Bernal L, Kang C-K, Shyy W (2009) Shallow and deep dynamic stall for flapping low Reynolds number airfoils. Exp Fluids 46(5):883-901
    • (2009) Exp Fluids , vol.46 , Issue.5 , pp. 883-901
    • Ol, M.V.1    Bernal, L.2    Kang, C.-K.3    Shyy, W.4
  • 12
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    • Stereo PIV measurement of a finite, flapping rigid plate in hovering condition
    • Suryadi A, Ishii T, Obi S (2010) Stereo PIV measurement of a finite, flapping rigid plate in hovering condition. Exp Fluids 49(2):447-460
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.