Results 31 to 40 of about 94,894 (308)

Investigation of Tip Leakage Vortex Structure and Trajectory in a Centrifugal Pump with a New Omega Vortex Identification Method

open access: yesApplied Sciences, 2022
Semi-open centrifugal pumps are widely used in various fields. However, the tip leakage vortex (TLV) has a malign effect on the impeller flow field.
Bing Qian   +5 more
doaj   +1 more source

Effect of rotor blade tip clearance on aerodynamic performance of high-speed multi-stage axial compressor

open access: yesNihon Kikai Gakkai ronbunshu, 2023
Using a high-speed multistage scale model compressor simulating a middle stage of a gas turbine compressor for power generation, the effects of 3 types of rotor tip clearances on performance and operating range, and the vortex structure of rotor tip ...
Ryosuke SEKI
doaj   +1 more source

Flow behaviors in a Kaplan turbine runner with different tip clearances

open access: yesAdvances in Mechanical Engineering, 2021
Tip clearance between the runner blade tip and shroud in a Kaplan turbine is inevitable, and the tip leakage flow (TLF) and tip leakage vortex (TLV) induced by the tip clearance have a considerable effect on the flow behaviors.
Yue Ma   +6 more
doaj   +1 more source

Numerical Analysis of the Effects of Different Rotor Tip Gaps in a Radial Turbine Operating at High Pressure Ratios Reaching Choked Flow

open access: yesEnergies, 2022
To operate, radial turbines used in turbochargers require a minimum tip gap between the rotor blades and the stationary wall casing (shroud). This gap generates leakage flow driven by the pressure difference between the pressure and suction side. The tip
José Galindo   +4 more
doaj   +1 more source

Generation Mechanisms of Rotating Stall and Surge in Centrifugal Compressors. [PDF]

open access: yes, 2017
Flow instabilities such as Rotating Stall and Surge limit the operating range of centrifugal compressors at low mass-flow rates. Employing compressible Large Eddy Simulations (LES), their generation mechanisms are exposed.
Mihăescu, Mihai   +2 more
core   +1 more source

Impact of Cooling Injection on the Transonic Over-Tip Leakage Flow and Squealer Aerothermal Design Optimization [PDF]

open access: yes, 2015
In the present work, the effect of coolant injection on the over-tip-leakage (OTL) flow and squealer designs has been investigated in a transonic flow regime.
He, L., Liu, Y., Wang, Z., Zhang, Q.
core   +1 more source

On scaling method to investigate high-speed over-tip-leakage flow at low-speed condition [PDF]

open access: yes, 2017
Modern high-pressure turbine blades operate at high-speed conditions. The over-tipleakage (OTL) flow can be high-subsonic or even transonic. From the consideration of problem simplification and cost reduction, the OTL flow has been studied extensively in
He, L., Jiang, H., Wang, L., Zhang, Q.
core   +1 more source

Flow Characteristics and Loss Mechanism of Tip Leakage Flow in Mining Contra-Rotating Axial Flow Fan

open access: yesApplied Sciences
Tip leakage flow interacts with the mainstream, impacting the energy transmission process within the impeller of the fan and causing a significant flow loss.
Yongping Chen   +3 more
doaj   +1 more source

Blade Tip Leakage Flow and Heat Transfer With Pressure-Side Winglet [PDF]

open access: yesVolume 5: Turbo Expo 2003, Parts A and B, 2003
A numerical study has been conducted to explore the effect of a pressure-side winglet on the flow and heat transfer over a blade tip. Calculations are performed for both a flat tip and a squealer tip. The winglet is in the form of a flat extension, and is shaped in the axial chord direction to have the maximum thickness at the chord location where the ...
A. K. Saha   +3 more
openaire   +2 more sources

Influences of tip leakage flows on flow field at design condition in transonic centrifugal compressor with splitter blade

open access: yesNihon Kikai Gakkai ronbunshu, 2016
A tip leakage flow is well known to have predominant influence on a loss generation in a compressor. An impeller for a transonic centrifugal compressor is generally composed of the main and the splitter blades to gain the choke flow rate.
Masanao KANEKO, Hoshio TSUJITA
doaj   +1 more source

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