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Volumn 45, Issue 3, 2000, Pages 157-164

Interaction of tip-vortices in the wake of a two-bladed rotor in axial flight

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW; COMPUTATIONAL FLUID DYNAMICS; FLIGHT DYNAMICS; MATHEMATICAL MODELS; TURBOMACHINE BLADES; VORTEX FLOW; WAKES;

EID: 0034228852     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/JAHS.45.157     Document Type: Article
Times cited : (29)

References (23)
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  • 4
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    • Gray, R.B.1
  • 5
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    • Challenges in understanding the vortex dynamics of helicopter rotor wakes
    • Leishman, J. G. and Bagai, A., "Challenges in Understanding the Vortex Dynamics of Helicopter Rotor Wakes," AIAA Journal, Vol. 36, No. 7, 1998, pp. 1130-1140.
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    • Leishman, J.G.1    Bagai, A.2
  • 6
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    • October
    • Landgrebe, A. J., "The Wake Geometry of a Hovering Rotor and its Influence on Rotor Performance," Journal of American Helicopter Society, Vol. 17, No. 4, October 1972, pp. 3-15.
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  • 8
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    • A prescribed wake lifting surface hover performance analysis
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    • Kocurek, J.D.1    Tangler, J.L.2
  • 10
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    • The steady motion and stability of a helical vortex
    • Levy, H. and Forsdyke, A. G., "The Steady Motion and Stability of a Helical Vortex," Proceedings Royal Society A, Vol. 120, 1928, pp. 670-690.
    • (1928) Proceedings Royal Society A , vol.120 , pp. 670-690
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  • 11
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  • 15
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    • Vorticity concentration at the edge of the inboard vortex sheet
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.