[HTML][HTML] Development and loss mechanism of turbine secondary flows at a low Reynolds number: A synergy analysis

Z Shao, H Zhang, R Wang - Physics of Fluids, 2023 - pubs.aip.org
To further explore the development of turbine secondary flows and associated losses at a
low Reynolds number, a synergy analysis was developed and implemented. Loss is defined …

Experimental investigation of total pressure loss development in a highly loaded low-pressure turbine cascade

P Bear, M Wolff, A Gross… - Journal of …, 2018 - asmedigitalcollection.asme.org
Improvements in turbine design methods have resulted in the development of blade profiles
with both high lift and good Reynolds lapse characteristics. An increase in aerodynamic …

Nonuniform height endwall fence optimization of a low-pressure turbine cascade

H Yuan, Y Wu, S Zhou, M Wang, X Lu… - International Journal of …, 2023 - Elsevier
As the lift of turbine increases, the secondary flow in the endwall region seriously restricts
improvement of the aerodynamic performance of low-pressure turbine. The particle swarm …

Active flow control for low-pressure turbines

J Bons, S Benton, C Bernardini, M Bloxham - AIAA Journal, 2018 - arc.aiaa.org
Recent applications of active flow control to the low-pressure turbine section of a gas turbine
are reviewed and evaluated. Unique aspects of the low-pressure turbine flow environment …

Aerodynamic performance of profiled endwalls with upstream slot purge flow in a linear turbine cascade having pressure side separation

S Babu, S Anish - Physics of Fluids, 2021 - pubs.aip.org
In aeroengines, purge flow directly fed from the compressor (which bypasses the combustor)
is introduced through the disk space between blade rows to prevent the hot ingress. Higher …

Experimental and numerical characterization of flow through highly loaded low-pressure turbine cascade

A Gross, CR Marks, R Sondergaard, PS Bear… - Journal of Propulsion …, 2018 - arc.aiaa.org
An increase in loading of low-pressure turbine blades beyond the present state of the art will
directly translate into lighter, smaller, and lower-cost turbine engines. Advances in …

Effects of the installation location of a dielectric barrier discharge plasma actuator on the active passage vortex control of a turbine cascade at low Reynolds numbers

T Matsunuma - Actuators, 2022 - mdpi.com
Because axial flow turbines are widely used as the main components of jet engines and
industrial gas turbines, their energy reduction effect is significant, even with a slight …

[HTML][HTML] Active Flow Control for Passage Vortex Reduction in a Linear Turbine Cascade with Various Tip Clearance Sizes Using a Dielectric Barrier Discharge Plasma …

T Matsunuma, T Segawa - Aerospace, 2023 - mdpi.com
In an axial-flow turbine of a jet engine used for aircraft propulsion, the passage vortex (PV)
and tip leakage vortex (TLV) generated inside the blade passage deteriorate the …

[HTML][HTML] Controlling secondary flow in high-lift low-pressure turbine using boundary-layer slot suction

QU Xiao, LI Liunan, Y Zhang, LU Xingen… - Chinese Journal of …, 2024 - Elsevier
The design of high-lift Low-Pressure Turbines (LPTs) causes the separation of the boundary
layer on the suction side of the blade and leads to a strong secondary flow. This present …

Unsteady effects of periodic wake passing frequency on aerodynamic performance of ultra-high-lift low pressure turbine cascades

X Qu, Y Zhang, X Lu, J Zhu - Physics of fluids, 2019 - pubs.aip.org
Flow losses and flow field data downstream of an ultra-high-lift aft-loaded low pressure
turbine cascade were comprehensively measured for different incoming wake passing …