Numerical Simulation of Separation Control for a Transitional Highly-Loaded Low-Pressure Turbine

Author:

Rizzetta Donald1,Visbal Miguel1

Affiliation:

1. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Reference66 articles.

1. S s d s=d xj Bons et al.10-12Sondergaard et al.131.13 5:56×1025:56×10310.0 0.63

2. Sondergaard et al.150.56-1.13 1.12 0.112 10.0 0.45

3. Table 2. Computational mesh spacings in wall units. Grid Points Processors ∆t+∆l+min ∆l+max ∆n+min ∆z+min ∆z+max coarse 5:3×10698 0.04 1.14 49.48 0.30 6.50 6.50

4. Experimental investigations10-13,15have used several parameters to describe characteristics of unsteady vortex generating jets. The jet blowing ratio B is defined as

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