Analysis of vortical flow field in a propeller fan by LDV measurements and LES—Part II: Unsteady nature of vortical flow structures due to tip vortex breakdown

Journal of Fluids Engineering, Transactions of the ASME

Volumn 123, Issue 4, 2001, Pages 755-761

  Jang, Choon Man ^a   Furukawa, Masato ^a   Inoue, Masahiro ^a  

^a KYUSHU UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 13344278721     PISSN: 00982202     EISSN: 1528901X     Source Type: Journal    
DOI: 10.1115/1.1412566     Document Type: Article

References (16)

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3. Furukawa, M., Inoue, M., Saiki, K., and Yamada, K., 1999, “The Role of Tip Leakage Vortex Breakdown in Compressor Rotor Aerodynamics,” ASME J. Turbomach., 121, No. 3, pp. 469-480.
4. Furukawa, M., Saiki, K., Yamada, K., and Inoue, M., 2000, “Unsteady Flow Behavior Due to Breakdown of Tip Leakage Vortex in an Axial Compressor Rotor at Near-Stall Condition,” ASME Paper No. 2000-GT-0666.
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