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The tip clearance is an essential structure in multiphase pumps, and the vortex flow caused by the leakage at the tip of the blade disturbs the internal flow field of the pump, leading to energy losses, which in turn weaken the pump’s pressure‐boosting performance and reduce its work output efficiency. To clarify the energy loss behavior at various tip
Zongku Liu +7 more
wiley +1 more source
Tip-leakage-flow excited unsteadiness and associated control [PDF]
Tip leakage flow in turbomachinery inherently generates intense unsteady features, named self-excited unsteadiness, which significantly affects the operating stability, aerodynamic efficiency, and noise but has not been well understood.
Möller, Felix +7 more
core +1 more source
Cavity width and height are two key geometric parameters of squealer tips, which could affect the control effect of squealer tips on tip leakage flow (TLF) of gas turbines.
Yufan Wang +4 more
doaj +1 more source
UEG Week 2022 Poster Presentations
United European Gastroenterology Journal, Volume 10, Issue S8, Page 473-1092, October 2022.
wiley +1 more source
Large Tip Clearance Flows in High Pressure Stages of Axial Compressors [PDF]
This thesis investigates over tip leakage where the tip clearance is large. In the high pressure stages of axial compressors the tip clearance can be typically 6% of span and the total blockage due to tip clearance can consume in excess of forty percent ...
WILLIAMS, RICHARD,JAMES
core
ABSTRACT High‐pressure turbine blade tips operate under extreme thermal stress, generating significant aerodynamic losses that must be continually optimized to improve engine efficiency and durability. This study uses computational fluid dynamics (CFD) to investigate the aerodynamic and thermal behavior of advanced turbine blade tip configurations ...
Kheir‐Eddine Arrif +2 more
wiley +1 more source
Tip Leakage Cavitation, Associated Bubble Dynamics, Noise, Flow Structure and Effect of Tip Gap Size [PDF]
This paper focuses on the onset of tip-leakage cavitation on a fixed hydrofoil. The objectives are to investigate the effect of gap size on the flow structure, conditions of cavitation inception, the associated bubble dynamics and cavitation noise.
Gopalan, Shridhar +2 more
core
Tip leakage flow structure and cavitation inception in a ducted marine propeller
Cavitation inception and the associated flow structure in the tip region of a ducted propeller are investigated experimentally at varying advance ratios (J) using high-speed imaging and stereoscopic particle image velocimetry (SPIV) measurements in a ...
Ayush Saraswat +3 more
doaj +1 more source
Unsteady characteristics analysis of compressors based on the proper orthogonal decomposition method [PDF]
An aero-engine is often accompanied by a strong unsteady flow at near-stall condition, and increasing unsteady airflow eventually makes the engine unstable. To explore the unsteady flow characteristics, the Rotor 37 was taken as the research object.
Shan Ma +4 more
doaj +1 more source
Numerical and Experimental Investigations of Axial Flow Fan with Bionic Forked Trailing Edge
To improve the performance of the aerodynamic properties and reduce the aerodynamic noise of an axial flow fan in the outdoor unit of an air conditioner, this study proposed a bionic forked trailing-edge structure inspired by the forked fish caudal fin ...
Zhong Liang +5 more
doaj +1 more source

