论文部分内容阅读
LES (Large-Eddy Simulation) computations were preformed to investigate the mechanisms of a kind of spanwisegroove for the passive control of laminar separation bubble on the suction surface of a low-speed highly loadedlow-pressure turbine blade at Re = 50,000 (Reynolds number, based on inlet velocity and axial chord length).Compared with the smooth suction surface, the numerical results indicate that: (1) the groove is effective toshorten and thin the separation bubble, which contributes the flow loss reduction on the groove surface, by thinningthe boundary layer behind the groove and promoting earlier transition inception in the separation bubble; (2)upstream movement of the transition inception location on the grooved surface is suggested being the result of thelower frequency at which the highest amplification rate of instability waves occurs, and the larger initial amplitudeof the disturbance at the most unstable frequency before transition; and (3) the viscous instability mode ispromoted on the grooved surface, due to the thinning of the boundary layer behind the groove.
LES (Large-Eddy Simulation) computations were preformed to investigate the mechanisms of a kind of spanwise motion for the passive control of laminar separation bubble on the suction surface of a low-speed highly loaded low-pressure turbine blade at Re = 50,000 (Reynolds number, based on inlet velocity and axial chord length. Compared with the smooth suction surface, the numerical results that that: (1) the groove is effective toshorten and thin the separation bubble, which contributes the flow loss reduction on the groove surface, by thinningthe boundary layer behind the groove and promoting earlier transition inception in the separation bubble; (2) upstream movement of the transition inception location on the grooved surface is suggested being the result of the low frequency frequency which which the highest amplification rate of instability waves occurs, and the larger initial amplitudeof the disturbance at the most unstable frequency before transition; and (3) the viscous instability mode isp romoted on the grooved surface, due to the thinning of the boundary layer behind the groove.