On the vortex created by multiple blades joined at a hub

Aeronautical Journal

Volumn 110, Issue 1104, 2006, Pages 117-119

  Spalart, P R ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; METHOD OF MOMENTS; WINGS;

AEROFOIL FUNCTION; ANGULAR MOMENTUM; VORTEX;

TURBOMACHINE BLADES;

EID: 33644937242     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000001068     Document Type: Review

References (6)

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2. SPALART, P.R. On the motion of laminar wing wakes in a stratified fluid. J Fluid Mech, 1996, 327, pp 139-160.
3. PHILLIPS, W.R.C. AND GRAHAM, J.A.H. Reynolds-stress measurements in a turbulent trailing vortex. J Fluid Mech, 1984, 147, pp 353-371.
4. BANDYOPADHYAY, P.R., STEAD, D.J. and ASH, R. L. Organized nature of a turbulent trailing vortex. AIAA J, 1991, 29, (10), pp 1627-1633.
5. BENINATI, M.L. and MARSHALL, J.S. An experimental study of the effect of free-stream turbulence on a trailing vortex, Expts in Fluids, 2005, 38, pp 244-257.
6. POPPLETON, E.D. Effect of air injection into the core of a trailing vortex. J Aircr, 1971, 8, (8), pp 672-673.