2016
DOI: 10.1007/s40430-016-0680-x
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Influence of the vortex design method in the performance characteristics of reversible axial rotors

Abstract: the main aerodynamic performance characteristics of these two rotors were determined, for a specific rotation, within a wide range of operation conditions. The non-free vortex rotor showed a higher maximum efficiency when compared to the free-vortex one, which was located in the region of stability of the rotor. On the contrary, the free-vortex rotor maximum efficiency was located in the region of instability of the rotor.

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Cited by 7 publications
(4 citation statements)
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“…The 2nd order upwind scheme was used for the spatial discretization of all the equations including a transport term (i.e., momentum, energy, and turbulence), as well as the bounded 2nd order implicit for the time differencing, to achieve a good resolution. The turbulence model utilized was k-ω SST, in line with Espinosa Sarmiento et al, 2021;Ramirez Camacho;de Oliveira, 2020;Sarmiento;Camacho, 2017, along pressurebased solver-type, within coupled solution algorithm. It was necessary 30 iterations per time-step that in turn was equal to 2,228x10 -4 s. The convergence criteria equal to 0,1% of variation in Coefficient of Power (Cp) between two subsequent revolutions is achieved at approximately 90 revolutions, so it was necessary 28880 time-steps.…”
Section: Solver Settingsmentioning
confidence: 99%
“…The 2nd order upwind scheme was used for the spatial discretization of all the equations including a transport term (i.e., momentum, energy, and turbulence), as well as the bounded 2nd order implicit for the time differencing, to achieve a good resolution. The turbulence model utilized was k-ω SST, in line with Espinosa Sarmiento et al, 2021;Ramirez Camacho;de Oliveira, 2020;Sarmiento;Camacho, 2017, along pressurebased solver-type, within coupled solution algorithm. It was necessary 30 iterations per time-step that in turn was equal to 2,228x10 -4 s. The convergence criteria equal to 0,1% of variation in Coefficient of Power (Cp) between two subsequent revolutions is achieved at approximately 90 revolutions, so it was necessary 28880 time-steps.…”
Section: Solver Settingsmentioning
confidence: 99%
“…This work will use a type of non-free vortex based on Wallis (1983) and Sarmiento et al (2017), where the circumferential component of the absolute velocity after the rotor, cu6, varies linearly along the blade. This condition is represented by Eq.…”
Section: Radial Equilibrium Conditionmentioning
confidence: 99%
“…One of the technologies used for power generation involves gas microturbines (GM), which produce a nominal power between 25 kWe and 300 kWe [11]. The structural configuration of turbines may vary according to the manufacturer and its application [12], but GM usually operates in a single-shaft configuration with a regeneration system, reaching efficiencies of up to 35%. In the case of GM without a regeneration mechanism, the electrical efficiency can reach values up to 17% [13].…”
Section: Introductionmentioning
confidence: 99%