The influence of downstream passage on the flow within an annular s-shaped duct

Journal of Turbomachinery

Volumn 120, Issue 4, 1998, Pages 714-722

  Sonoda, T ^a   Arima, T ^a   Oana, M ^a  

^a HONDA R AND D CO LTD   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; NAVIER STOKES EQUATIONS; PRESSURE DROP; REYNOLDS NUMBER; TURBOFAN ENGINES; TURBULENCE;

ANNULAR S-SHAPED DUCTS; DOWNSTREAM PASSAGE;

DUCTS;

ANNULAR FLOW; CENTRIFUGAL COMPRESSOR; DUCT; FLOW SEPARATION; S-TYPE TURBINE;

EID: 0032194378     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841782     Document Type: Article

References (6)

1. Arima, T., Sonoda, T., Shirotori, M., Tamura, A., and Kikuti, K., 1997, “A Numerical Investigation of Transonic Axial Compressor Rotor Flow Using a Low Reynolds Number k-e Turbulence Model,” ASME Journal of Turbomachinery, in press
2. Bailey, D. W., and Carrotte, J. F., 1996, “The Influence of Inlet Swirl on the Flow Within an Annular S-Shaped Duct,” ASME Paper No. 96-GT-60.
3. Bailey, D. W., Britchford, J. F., Carrotte, J. F., and Stevens, S. J., 1997, “Performance Assessment of an Annular S-Shaped Duct,” ASME Journal of Turbomachinery, Vol. 119, pp. 149-156.
4. Britchford, K. M., Carrotte, J. F., Stevens, S. J., and McGuirk, J. J., 1994, “The Development of the Mean Flow and Turbulence Structure in an Annular S-Shaped Duct,” ASME Paper No. 94-GT-457.
5. Denton, J, D., 1985, “The Calculation of Fully 3D Flow Through Any Type of Turbomacbine Blade Row,” AGARD Lecture Series—-3D Computational Techniques Applied to Internal Flows in Propulsion Systems, AGARD LS 140.
6. Karim Abdulla-Altaii, A., and Raj, R, S., 1994, “Secondary Flow Development Downstream of a Blade Endwall Corner,” ASME Paper No. 94-GT-459.