2019
DOI: 10.1016/j.ast.2019.04.002
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Numerical investigation on the biomimetic trailing edge of a high-subsonic turbine blade

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Cited by 21 publications
(7 citation statements)
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“…al [18], Melzer and Pullan pointed out that the use of an elliptic trailing edge shape will both increase and equalize the base pressure, suppressing transonic vortex shedding for those conditions where straight or slightly rounded trailing edges would develop it. Luo et al [19] proposed a biomimetic spanwise trailing edge shape that was able to eliminate the shedding of von Kármán vortices, transforming them into small three-dimensional vortices that would quickly dissipate reducing the mixing losses. Different ways to control the flow over turbine airfoils have been considered in the last decades.…”
Section: Introductionmentioning
confidence: 99%
“…al [18], Melzer and Pullan pointed out that the use of an elliptic trailing edge shape will both increase and equalize the base pressure, suppressing transonic vortex shedding for those conditions where straight or slightly rounded trailing edges would develop it. Luo et al [19] proposed a biomimetic spanwise trailing edge shape that was able to eliminate the shedding of von Kármán vortices, transforming them into small three-dimensional vortices that would quickly dissipate reducing the mixing losses. Different ways to control the flow over turbine airfoils have been considered in the last decades.…”
Section: Introductionmentioning
confidence: 99%
“…Although it is proved that the bionic trailing edge can suppress the Karman vortex and reduce wake loss significantly at an exit Mach number of 0.79 in (Luo et al, 2019), as mentioned above, different exit Mach numbers have a great influence on the form of trailing edge vortex for conventional blades, so the important purpose of this paper is to study the influence of the BTE on the wake vortex and the ability to control wake loss under different Mach number conditions (0.38-1.21), especially after the Mach number is greater than 1, and the influence of BTE on the shockwave system and related loss. This study provides an important reference for the application of BTE in turbines under different working conditions.…”
Section: Introductionmentioning
confidence: 99%
“…Besides this, a more convex curvature can suppress the vortex shedding, and the trailing edge loss was lower. Inspired by the whisker of the harbor seal, the authors propose a bionic method to control the vortex shedding at the trailing edge of turbine blades (Luo et al, 2019).…”
Section: Introductionmentioning
confidence: 99%
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“…Li et al [21] studied the influences of sinusoidal tubercle trailing edge (STTE) impeller on the unstable pressure pulsation of centrifugal pumps and concluded that the STTE impeller can reduce the pressure pulsation amplitude. Luo et al [22] investigated the mechanism of wake loss reduction for biomimetic trailing edge and concluded that the wake area for the biomimetic trailing edge case is narrow, and the velocity in the wake recovers more quickly compared with the situations in the three other cases. Valipour et al [23] used a parameterised perturbation method to solve the corresponding nonlinear differential equation.…”
Section: Introductionmentioning
confidence: 99%