This paper presents an experimental investigation of the control of airfoil aerodynamics at a
low Reynolds number of 5× 10 4 within a wide range of attack angle α using a leading-edge …

From takeoff to cruise, the operating Reynolds number (Re) of the low-pressure turbine
(LPT) in an aero-engine decreases significantly, making the boundary layer near the aft …

Boundary layer separation control has been studied using vortex generator jets (VGJs) on a
very high lift, low-pressure turbine airfoil. Experiments were done under low (0.6%) …

WITH the trend toward higher bypass ratios in turbofans, demands are increasing for the low-
pressure turbines (LPTs) that drive the large fan assemblies. Also, many military and civilian …

Mixed flow fan is a kind of widely used turbomachine, which has faced problems of further
performance improvement in traditional design methods in recent decades. Inspired by the …

Boundary layer separation, transition, and reattachment have been studied on a new, very
high lift, low-pressure turbine airfoil. Experiments were done under low freestream …

Modern high-performance low-pressure turbines (LPT) usually encounter flow problems at
low Reynolds numbers, especially for high-altitude UAVs under cruise conditions. Flow …

Boundary layer separation control has been studied using vortex generator jets (VGJs) on a
very high lift, low-pressure turbine airfoil. Experiments were done under high (4%) …

Through experiments using two-dimensional particle-image velocimetry (PIV), this paper
examines the nature of transition in a separation bubble and manipulations of the resultant …

This paper addresses the issue of aerodynamic performance of a novel 3D leading edge
modification to a reference low pressure turbine blade. An analysis of tubercles found in …