An efficient numerical method for highly loaded transonic cascade flow
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering,General Mathematics
Link
http://link.springer.com/content/pdf/10.1007/s10665-007-9150-x.pdf
Reference21 articles.
1. Curtis EM, Hodson HP, Banieghbal MR, Denton JD, Howell RJ and Harvey NW (1996). Development of blade profiles for low pressure turbine applications. ASME J Turbomach 119(3): 531–538
2. Chima RV (1996). Application of the k-omega turbulence model to quasi-three-dimensional turbomachinery flows. J Propulsion Power 12(6): 1176–1179
3. Gehrer A, Jericha H (1998) External heat transfer predictions in a highly-loaded transonic linear turbine guide vane cascade using an upwind biased Navier–Stokes solver. ASME Paper 98-GT-238
4. Hall U, Larsson J, Bario F, Kulisa P, Slimani J, Begin V, Eriksson L-E, Wahlen U (1998) Simulations and measurements on impulse blades for heat transfer prediction in supersonic turbine applications. ASME 98-GT-154, International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden
5. Howell RJ, Hodson HP, Schulte V, Stieger RD, Heinz-Peter S, Hasslebach F and Harvey NW (2002). Layer development in the BR710 and BR715 LP turbines—the implementation of high lift and ultra high lift concepts. J Turbomach 124(3): 385–392
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