Results 21 to 30 of about 9,981 (232)

On the challenge of five-hole-probe measurements at high subsonic Mach numbers in the wake of transonic turbine cascades

open access: yesJournal of the Global Power and Propulsion Society, 2018
Five-hole-probes are common use in turbomachinery flow investigations, even though, inserting a probe into a flow field inevitably induces perturbations to the flow which can falsify the measurement results, especially when exposed to transonic flows ...
Marcel Boerner   +2 more
doaj   +1 more source

CFD Simulation of Transonic Flow Through the Tip-Section Turbine Blade Cascade Intended for the Long Turbine Blade [PDF]

open access: yesMATEC Web of Conferences, 2022
The paper deals with numerical simulations of transonic flow through the turbine blade cascade consisting of flat profiles. The cascade is one of variants of the tip section of ultra-long blades, which were designed for the last stage of the steam ...
Kosiak Pavlo   +3 more
doaj   +1 more source

Investigation on Transonic Characteristics of Turbine Cascades.

open access: yesTRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, 1998
Transosic characteristics of three similar turbine cascades (designed for same condition, but with slightly different curvature of blade suction surface after throat) were tested by high-speed cascade wind tunnel. Experimental data showed small difference of curvature of blade suction surface after throat affected loss coefficient in transonic region ...
Hidenori YOSHIDA   +3 more
openaire   +2 more sources

Aerodynamic Damping Characteristics of a Transonic Turbine Cascade [PDF]

open access: yesVolume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award; General, 1999
The unsteady aerodynamic characteristics of oscillating thin turbine blades were studied both experimentally and numerically to obtain the comprehensive knowledge on the aerodynamic damping of the blades operating in transonic flows. The experiment was carried out in a linear cascade tunnel by use of the influence coefficient method.
Mizuho Aotsuka   +2 more
openaire   +1 more source

Three-Dimensional, Unsteady, Inviscid Flow in an Axial Turbine Stage [PDF]

open access: yesEngineering and Technology Journal, 2009
This paper presents an advanced approach to compute the three-dimensional,rotational, adiabatic, inviscid flow of a perfect gas in a highly twisted transonic axial turbinestage.
Abdulhassan A. Karamallah   +2 more
doaj   +1 more source

Experimental and numerical study on condensation in transonic steam flow

open access: yesOpen Engineering, 2015
The present paper describes an experimental and numerical study of steam condensing flow in a linear cascade of turbine stator blades. The experimental research was performed on the facility of a small scale steam power plant located at Silesian ...
Majkut Mirosław   +3 more
doaj   +1 more source

Numerical modelling of turbulent transition in complex geometries

open access: yesEPJ Web of Conferences, 2018
The work deals with numerical simulation of laminar-turbulent transition in transonic flows in turbine cas-cades. The 3D cascade geometry as well as 2D model cascade in a wind tunnel is simulated.
Louda Petr   +2 more
doaj   +1 more source

Investigation of unsteady flow in axial turbine stage

open access: yesEPJ Web of Conferences, 2012
The never ending process to increase the efficiency of turbine stages introduced an idea to create an axial turbine stage test rig as part of closed loop transonic wind tunnel at Vyzkumny a zkusebni letecky ustav (VZLU).
Němec Martin, Jelínek Tomáš
doaj   +1 more source

Blowing jets as a circulation flow control to enhancement the lift of wing or generated power of wind turbine [PDF]

open access: yesINCAS Bulletin, 2014
The goal of this paper is to provide a numerical flow analysis based on RANS equations in two directions: the study of augmented high-lift system for a cross-section airfoil of a wing up to transonic regime and the circulation control implemented by ...
Alexandru DUMITRACHE   +3 more
doaj   +1 more source

Pressure Bifurcation Phenomenon on Supersonic Blowing Trailing Edges

open access: yes, 2018
Turbine blades operating in transonic-supersonic regime develop a complex shock wave system at the trailing edge, a phenomenon that leads to unfavorable pressure perturbations downstream and can interact with other turbine stages. Understanding the fluid
de Vicente, Javier   +3 more
core   +3 more sources

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