Results 31 to 40 of about 93,522 (307)

A novel approach for suppressing leakage flow through turbine blade tip gaps

open access: yesPropulsion and Power Research, 2022
Tip clearance leakage flow of the turbine bade is an important factor limiting the augment of the high pressure turbine efficiency, which should be suppressed utilizing certain methods.
Tianyi Wang, Yimin Xuan
doaj   +1 more source

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

Blade Loading Effects on Axial Turbine Tip Leakage Vortex Dynamics and Loss [PDF]

open access: yes, 2012
umerical simulations have been carried out to define the loss generation mechanisms associated with tip leakage in un-shrouded axial turbines. Tip clearance vortex dynamics are a dominant feature of two mechanisms important in determining this loss: (i ...
Clemens, E. F.   +5 more
core   +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

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

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

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

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

Numerical analysis of secondary flow topologies of low-speed axial fans from compressor to load-controlled windmill [PDF]

open access: yes, 2017
mode to loaded windmill. A first objective is to identify generic patterns of rotor separation topology at windmill and bring light on the mechanisms responsible for it.
Binder, Nicolas   +4 more
core   +1 more source

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