DOI: 10.11606/d.8.2001.tde-29052002-094254
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O niilismo de Schopenhauer.

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“…The longitudinal distribution of the vortex intensity is shown in Figure 14 for a velocity of 0.4 m/s and Figure 15 for a velocity of 2.0 m/s. In the case of CRWP and RWP, the longitudinal vortex intensity tends to dissipate after passing VGs due to viscous effects [2,26,28]. Therefore, the installation of the second and third rows of VG reinforces the intensity of the longitudinal vortex as illustrated in Figures 12(c)-(f) and Figures 13(c)-(f) for velocities of 0.4 m/s and 2 m/s, respectively.…”
Section: Longitudinal Vortex Intensitymentioning
confidence: 86%
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“…The longitudinal distribution of the vortex intensity is shown in Figure 14 for a velocity of 0.4 m/s and Figure 15 for a velocity of 2.0 m/s. In the case of CRWP and RWP, the longitudinal vortex intensity tends to dissipate after passing VGs due to viscous effects [2,26,28]. Therefore, the installation of the second and third rows of VG reinforces the intensity of the longitudinal vortex as illustrated in Figures 12(c)-(f) and Figures 13(c)-(f) for velocities of 0.4 m/s and 2 m/s, respectively.…”
Section: Longitudinal Vortex Intensitymentioning
confidence: 86%
“…From Figures 10 and 11, it is observed that the longitudinal vortex in the X1 plane is stronger than that in the X2 plane for all types of VG with/without holes. This is due to viscous dissipation, which causes the longitudinal vortex to gradually weaken as the flow away from VG [28]. In the X3 plane, the longitudinal vortex strength increases compared to the X2 plane due to the addition of VGs, which results in an increase in fluid velocity in the downwash region [29].…”
Section: Flow Fieldmentioning
confidence: 99%