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Generation and Development of Klebanoff Streaks in Low-Pressure Turbine Cascade Under Upstream Wakes
Publikováno v:
Volume 2B: Turbomachinery.
At low Reynolds numbers operating condition, the boundary layer of the high-lift low-pressure turbine (LPT) of aero-engines is prone to separate on the suction surface of the airfoil. The profile losses of the airfoil are largely governed by the size
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ca2f66370d9890ff1c358e660a89a1e1
https://doi.org/10.1115/gt2020-15313
https://doi.org/10.1115/gt2020-15313
