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Research Conducted by F. Satta and Co-Researchers Has Updated Our Knowledge about Propulsion and Power (Loading Distribution Effects on Separated...

July 2, 2014



Research Conducted by F. Satta and Co-Researchers Has Updated Our Knowledge about Propulsion and Power (Loading Distribution Effects on Separated Flow Transition of Ultra-High-Lift Turbine Blades)

By a News Reporter-Staff News Editor at Defense & Aerospace Week -- Current study results on Propulsion and Power have been published. According to news reporting originating from Turin, Italy, by VerticalNews correspondents, research stated, "The suction side boundary-layer evolution in two ultra-high-lift low-pressure turbine blade cascades, characterized by the same Zweifel number but two different aerodynamic loading distributions, has been experimentally analyzed under steady and unsteady incoming flows. For the steady inflow case, a suction side boundary-layer separation has been detected for both cascades."

Our news editors obtained a quote from the research, "Time-mean velocity and unresolved unsteadiness distributions have been exploited to survey the dynamics of the separated flow transition mode. The spectral analysis reveals that only the midloaded cascade is affected by a Kelvin-Helmholtz instability that induces the separated shear layer rollup, which provokes high losses. Results obtained for the unsteady case reveal that linear stability mechanisms drive the amplification of velocity fluctuations carried by wakes with dynamics similar to that characterizing the steady inflow condition. A rollup vortex has been found to be generated for both cascades as a consequence of the wake shear-layer interaction process. Different vortex dimensions have been recognized in the two cases, due to the different shear layer thicknesses at separation."

According to the news editors, the research concluded: "The stronger and larger roll-up vortex characterizing the front-loaded cascade allows explaining the higher losses of this cascade, when it operates with unsteady inflow, as compared with the midloaded one."

For more information on this research see: Loading Distribution Effects on Separated Flow Transition of Ultra-High-Lift Turbine Blades. Journal of Propulsion and Power, 2014;30(3):845-856. Journal of Propulsion and Power can be contacted at: Amer Inst Aeronautics Astronautics, 1801 Alexander Bell Drive, Ste 500, Reston, VA 22091-4344, USA.

The news editors report that additional information may be obtained by contacting F. Satta, Avio Aero, I-10010 Turin, Italy. Additional authors for this research include D. Simoni, M. Ubaldi, P. Zunino and F. Bertini.

Keywords for this news article include: Turin, Italy, Europe, Propulsion and Power

Our reports deliver fact-based news of research and discoveries from around the world. Copyright 2014, NewsRx LLC


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Source: Defense & Aerospace Week


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