Results 71 to 80 of about 807 (188)

VIBRATION CHARACTERISTICS OF PRETWISTED AEROFOIL CROSS-SECTION BLADE PACKETS UNDER ROTATING CONDITIONS

open access: yes, 1992
Turbine blades are usually pretwisted and have asymmetric cross sections. Furthermore, turbine blades are formed into packets by joining them at critical locations with shrouds or lacing. Such a procedure alters the vibration characteristics of the blade.
THOMAS, J, SABUNCU, M
core   +1 more source

Rotating Instabilities in a Radial Vaneless Diffuser

open access: yes, 2010
The paper reports on the flow field in a vaneless diffuser of a radial flow pump at partial flow conditions. Experimental data were obtained within the diffuser using 2D/3C high repetition rate PIV coupled with unsteady pressure transducers. The pressure
DUPONT P   +6 more
core  

Formation and evolution of Rayleigh-Bénard streaks in rotating cavities

open access: yes, 2018
This paper presents numerical investigation into the phenomena of so-called Rayleigh-Bénard streaks inside rotating-cavities. Experimental data from the University of Sussex Multiple Cavity Rig (MCR) has been used as boundary conditions for Unsteady ...
Mark Puttock-Brown (4462249)   +1 more
core   +1 more source

Large-eddy simulation of buoyancy-induced flow in a sealed rotating cavity [PDF]

open access: yes, 2018
Buoyancy-induced flows occur in the rotating cavities of gas turbine internal air systems, and are particularly challenging to model due to the inherently unsteadiness of these flows.
Pitz, Diogo B   +3 more
core   +1 more source

Drag Reduction Effect of Gradually-Varying Riblet Structures on Conical Rotating Disks

open access: yes水下无人系统学报
Based on the enclosed flow field conditions and optimized dynamic-static clearances, a gradually-varying riblet drag reduction structure was proposed by combining the drag reduction principle of uniform-sized riblets to address the problem of increased ...
Sen WU, Jiaqi ZOU, Yicheng FAN, Dan ZHAO
doaj   +1 more source

Experimental and computational investigation of Rayleigh-Bénard flow in the rotating cavities of a core compressor

open access: yes, 2017
This paper presents new experimental measurements, at conditions representative of an aero engine, of heat transfer from the inner peripheral surface (shroud) of a rotating cavity.
Mark Puttock-Brown (4462249)   +2 more
core   +3 more sources

Comparaisons between numerical calculations and measurements in the vaned diffusor of SHF impeller [PDF]

open access: yes, 2012
The paper presents analysis of the performance and the internal flow behaviour in the vaned diffusor of a radial flow pump using PIV technique and pressure probe traverses.
ROUSSETTE, Olivier   +5 more
core  

Extension of the Rotating Disk Electrode Method to Thin Samples of Non-Disk Shape

open access: yes, 2019
A straightforward approach is presented to make thin electrode samples of non-disk shape compatible with the rotating disk electrode method, by merely attaching the sample on the rotating shroud and confining the area exposed to the electrolyte using ...
Katsounaros, Ioannis   +13 more
core   +1 more source

Repair of aircraft engine parts made of heat-resistant nickel alloys using additive plasma technologies

open access: yesАвіаційно-космічна техніка та технологія
In order to improve the maintainability of aircraft engine parts, the article examined the use of additive technologies in repairs. The article establishes that the use of additive technologies by the method of plasma surfacing in the repair of aircraft ...
Konstantin Balushok, Sergey Chigileychik
doaj   +1 more source

FREQUENCIES AND MODES OF ROTATING FLEXIBLE SHROUDED BLADED DISCS-SHAFT ASSEMBLIES

open access: yesTASK Quarterly, 2003
It is now increasingly necessary to predict accurately, at the design stage and without excessive computing costs, the dynamic behaviour of rotating parts of turbomachines, so that resonant conditions at operating speeds are avoided. In this study, global  rotating mode shapes of flexible shrouded bladed disc-shaft assemblies are calculated.
JACEK SOKOŁOWSKI   +2 more
openaire   +1 more source

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