Results 51 to 60 of about 807 (188)

Experimental Investigation of an Efficient and Lightweight Designed Counter-Rotating Shrouded Fan Stage [PDF]

open access: yesInternational Journal of Turbomachinery, Propulsion and Power
The German Aerospace Center designed, aero-mechanically optimized and experimentally investigated its own counter-rotating shrouded fan stage in the frame of the project CRISPmulti. Their target and the motivation of this work was, on the one hand, the generation of a highly accurate experimental database for the validation of the modern numerical ...
Lengyel-Kampmann, Timea   +3 more
openaire   +5 more sources

Comparative study on the complex behaviour of flow fields in a transparent non-axisymmetric corotating system between two arm-insertion angles at two measurement planes in an enclosure

open access: yesJournal of Fluid Science and Technology
Flow driven by co-rotating disks, such as hard disk drives (HDD) have been studied in previous research using axisymmetric models. In our work, a unique non-axisymmetric 3.5" transparent HDD model for information storage was used to investigate the ...
Ibrahim Abubakar MASUD   +3 more
doaj   +1 more source

POD-based frequency study of rotating stall in splitter pump-turbines [PDF]

open access: yesAIP Advances
Rotating stall (RS) compromises pump-turbine stability by inducing strong inter-blade flow separation and low-frequency pressure/velocity fluctuations, especially in the pumping hump region.
Qingyu Gu   +3 more
doaj   +1 more source

A Computational Study of a Novel Turbine Rotor Partial Shroud [PDF]

open access: yes, 2000
The over tip leakage (OTL) flow that exists between the stationary casing and the rotor tip of a shroudless HP turbine remains a major source of loss of performance for modern aero gas turbines. To-date the principal approaches to reducing OTL loss have
Neil W Harvey, Ken Ramsden
core  

Aerodynamic and Aerothermal Investigation of the Flow Around an HPT Rotor Shroud: Heat Transfer and Cooling Effectiveness

open access: yes, 2011
An experimental study has been conducted to investigate the aerothermal performance of a shrouded high pressure turbine blade in a large scale rotating rig. The rotor blade and the associated shroud and casing geometry have been modelled in a large scale
Howard Hodson   +5 more
core   +1 more source

Design and Performance Analysis of Contra-rotating Pumpjet Propulsor under Condition of Torque Unbalance

open access: yesMATEC Web of Conferences, 2018
In order to balance the torque of front rotor and rear rotor of underwater vehicle, the analysis of the speed triangles at the inlet and outlet of the front and rear rotor has been done.
Wang Xiao-er   +2 more
doaj   +1 more source

Experimental and CFD Studies of the Hydrodynamics in Wet Agglomeration Process

open access: yesChemEngineering, 2018
In this study, an experimentally validated computational model was developed to investigate the hydrodynamics in a rotor-stator vortex agglomeration reactor RVR having a rotating disc at the centre with two shrouded outer plates.
Benjamin Oyegbile   +2 more
doaj   +1 more source

Effect of Solidity on the Leakage Flow and Related Noise in Axial-Flow Fans with Rotating Shroud Operating at Fixed Performance

open access: yesInternational Journal of Turbomachinery, Propulsion and Power
This work presents an experimental study of the effect of blade count on the flow field and the radiated noise in a low-speed axial fan with a rotating shroud.
Tayyab Akhtar   +4 more
doaj   +1 more source

Deep Learning-assisted Fluid–structure Interaction for Fatigue Life Analysis of Slurry Pump Impellers in Particulate Two-phase Flow [PDF]

open access: yesJournal of Applied Fluid Mechanics
Slurry pump impellers operating in particulate solid–liquid flows often experience stress concentration and fatigue failure, limiting their reliability and service life.
Z. Liu, K. Peng, X. Lv, H. Chen, Z. Qu
doaj   +1 more source

Aerodynamic and Aerothermal Investigation of the Flow Around an HPT Rotor Shroud: PIV Measurements

open access: yes, 2012
An experimental study has been conducted to investigate the aerothermal performance of a shrouded high pressure turbine blade in a large scale rotating rig. The rotor blade and the associated shroud and casing geometry have been modelled in a large scale
Howard Hodson   +5 more
core   +1 more source

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