G circumferential places on the NGV downstream of your swirler. One particular can notice a a weak upstream effect downstream in the swirler. A single can notice weak upstream effect of areas from the on the NGV on the total pressure distribution in plane P40, that is positioned 42.five from the the NGV on the total pressure distribution in plane P40, which is located 42.five with the NGV NGV axial chord in front of cascade. That is constant with LESLES results the the FACaxial chord in front of cascade. This can be consistent with the the results for for Factor configuration Compound 48/80 supplier presented by [12], [12], who state substantial impact is noticed noticed 25 from the TOR configuration presented by who state that athat a significant influence isup to up to 25 axial axial The azimuthal NGV NGV position has an insignificant effect on pressure of thechord.chord. The azimuthalposition has an insignificant impact on the total the total distribution in plane P40. pressure distribution in plane P40.Figure ten. Normalized stress in P40. Figure 10. Normalized stress in P40.Some variations can be located if one compares the non-dimensional temperature Some variations is usually discovered if one compares the non-dimensional temperature distribution in this plane (Figure 11), but again, the azimuthal position in the NGV does distribution in this plane (Figure 11), but once again, the azimuthal position from the NGV will not drastically have an effect on the temperature at this axial place. Nonetheless, the primary flow not substantially have an effect on the temperature at this axial place. Nevertheless, the principle flow characteristics are extremely similar in all circumstances, with and without the need of NGV. The shape high-temperature options are extremely comparable in all instances, with and without having NGV. The shape of of high-temperazones is actually a outcome of clockwise vortex generated by the swirler. The rotation direction is ture zones is a resultaof a clockwise vortex generated by the swirler. The rotation direction indicated by the black arrow inside the contour plot in in Figure As shown above, the presence is indicated by the black arrow in the contour plot Figure 10.10. As shown above, the presof guide vanes weakly influences the the total pressure distribution YN968D1 Protein Tyrosine Kinase/RTK towards the end walls, ence of guide vanes weakly influencestotal stress distribution close close to the finish but is sufficient to act on the developed streamwise vortex and and to modify the temperwalls, but is adequate to act on the developed streamwise vortex to modify the temperature distribution by its stretching towards the hub. The place of your vortex and its evolution ature distribution by its stretching towards the hub. The location on the vortex and its at the inlet-to-blade passage is presented in Figure 12. The red zone shows the place of a higher worth of your axial vorticity component, which is deemed the main vortex representation, in contrast to blue zones, indicating counter-rotating vortices. The red zone indicates a good sense of rotation (black arrow in Figure ten), whilst the blue zone– unfavorable. The vortex is visualized by the axial component (z path) on the vorticityAerospace 2021, 8,evolution in the inlet-to-blade passage is presented in Figure 12. The red zone sho evolution in the inlet-to-blade passage is presented in Figure 12. The red zone sho place of a higher worth from the axial vorticity element, which is viewed as the place of a high value of your axial vorticity element, that is thought of the 12 of 16 vortex representation, in contrast to blue zones, indic.
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