| contributor author | Shuang Sun | |
| contributor author | Tianrong Tan | |
| contributor author | Xingshuang Wu | |
| contributor author | Xingen Lu | |
| contributor author | Yanfeng Zhang | |
| contributor author | Junqiang Zhu | |
| date accessioned | 2022-01-30T21:47:00Z | |
| date available | 2022-01-30T21:47:00Z | |
| date issued | 11/1/2020 12:00:00 AM | |
| identifier other | %28ASCE%29AS.1943-5525.0001193.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4268831 | |
| description abstract | The wake-induced transition, natural transition, and instability induced by the Klebanoff streaks complicate the transition process. In this paper, the boundary layer on the suction surface of a high-lift low-pressure turbine (LPT) was investigated at the design and +10° incidence with upstream wakes under numerical simulations and experiments. The interactions between the wakes and boundary on the leading edge of the blade at two incidences are mainly discussed. A positive incidence gives rise to an adverse pressure gradient (APG) over the forward suction surface. The adverse pressure gradient enhances the shear sheltering effect and, as a result, reduces penetration. However, strong Klebanoff streaks are amplified by the APG at +10° incidence and experience a weak viscous decay due to the moderately favorable pressure gradient (FPG). Between the wake passing events, weak Klebanoff streaks are also amplified by the APG at +10° incidence but barely amplified at 0° incidence. Klebanoff streaks appear almost in the whole wake passing cycle, resulting in an earlier transition onset and a longer transition process at +10° incidence. | |
| publisher | ASCE | |
| title | Influence of the Upstream Wakes on the Boundary Layer of a High-Lift Low-Pressure Turbine at Positive Incidence | |
| type | Journal Paper | |
| journal volume | 33 | |
| journal issue | 6 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0001193 | |
| page | 13 | |
| tree | Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 006 | |
| contenttype | Fulltext | |