Results 11 to 20 of about 93,460 (307)

Prediction of Tip-Leakage Losses in Axial Turbines [PDF]

open access: yesJournal of Turbomachinery, 1990
Existing methods for predicting the tip-leakage losses in turbomachinery are based on a variety of assumptions, many of which have not been fully verified experimentally. Recently, several detailed experimental studies in turbine cascades have helped to clarify the physics of the flow and provide data on the evolution of the losses.
M. I. Yaras, S. A. Sjolander
openaire   +1 more source

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

Effects of Loading Level on the Variation of Flow Losses in Subsonic Axial Compressors

open access: yesEnergies, 2022
The development of the aircraft industry seeks an increase in compressor loading, bringing unique flow phenomena and design problems; thus, insights into the ultrahigh loaded compressor are in great need.
Ruoyu Wang   +3 more
doaj   +1 more source

Effect of Film Position on the Flow and Heat Transfer Characteristics of Full-Ribbed Rotor Tip

open access: yesFrontiers in Energy Research, 2022
This article numerically studied the flow and heat transfer characteristics of the full-ribbed fluted tip of a rotor with four types of distribution of cooling films, namely, the mid-arc uniform film at the bottom of the groove, the uniform film on full ...
Haimeng Zhou   +4 more
doaj   +1 more source

Experimental study of endwall flow in a low-speed linear compressor cascade: effect of over-tip leakage [PDF]

open access: yes, 2017
This paper describes the study of endwall flow modification due to over-tip leakage flow in axial compressor blades. Un-shrouded axial compressor stator and rotor blades in aero-engines and land based gas turbines are subjected to over-tip leakage flow ...
Kanjirakkad, Vasudevan
core   +1 more source

Polarization retention loss in PbTiO3 ferroelectric films due to leakage currents [PDF]

open access: yes, 2007
The relationship between retention loss in single crystal PbTiO3 ferroelectric thin films and leakage currents is demonstrated by piezoresponse and conductive atomic force microscopy measurements.
A. Morelli   +5 more
core   +3 more sources

Effect of tip winglet position on tip flow and noise of axial flow fan

open access: yesHeliyon, 2023
In order to investigate the impact of blade tip winglet position on the internal flow and noise characteristics of axial flow fans,three different blade tip winglets,namely the TSW blade, the SSW blade, and the PSW blade,were hereby proposed.
Lei Diao   +5 more
doaj   +1 more source

Effect of pressurization on tip leakage losses in micro-scale centrifugal compressors

open access: yesEuropean Conference on Turbomachinery Fluid Dynamics and Thermodynamics, 2021
Turbomachinery miniaturization has been an emerging research field during the last decades and, especially, micro-scale radial compressors are becoming increasingly relevant due to the development of high-speed electric motors. They can be found in a wide range of applications such as micro gas turbines, aerial unmanned vehicles propulsion, fuel cells ...
Sebastián Herrera, Andrés   +2 more
openaire   +2 more sources

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

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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