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41st Aerospace Sciences Meeting and Exhibit
The numerical simulations for two sets of unsteady wake/blade interaction experiments are performed. The first experiment considered was conducted by Kaszeta et al. (2001) to study the effects of periodically passing wakes on transition and separation in a low pressure turbine passage. The second set of experiments considered are the linear turbine cascade experiments of Schobeiri and Pappu (1997) which were conducted to investigate the unsteady boundary layer behavior on a NASA Space Shuttledoi:10.2514/6.2003-1256 fatcat:nwskhlbhn5goljtbfs2gvrx4tm