[HTML][HTML] Uncertainty quantification in particle image velocimetry

A Sciacchitano - Measurement Science and Technology, 2019 - iopscience.iop.org
Particle image velocimetry (PIV) has become the chief experimental technique for velocity
field measurements in fluid flows. The technique yields quantitative visualizations of the …

Shock and shear layer interactions in a confined supersonic cavity flow

SK Karthick - Physics of Fluids, 2021 - pubs.aip.org
The impinging shock of varying strengths on the free shear layer in a confined supersonic
cavity flow is studied numerically using the detached eddy simulation. The resulting …

Unsteady Flows and Component Interaction in Turbomachinery

S Salvadori, M Insinna, F Martelli - International Journal of …, 2024 - mdpi.com
Unsteady component interaction represents a crucial topic in turbomachinery design and
analysis. Combustor/turbine interaction is one of the most widely studied topics both using …

Online analytics framework of sensor-driven prognosis and opportunistic maintenance for mass customization

T Xia, X Fang, N Gebraeel, L Xi… - Journal of …, 2019 - asmedigitalcollection.asme.org
In mass customization, a manufacturing line is required to be kept in reliable operation to
handle product demand volatility and potential machine degradations. Recent advances in …

Resolving nonuniform temperature distributions with single-beam absorption spectroscopy. Part I: Theoretical capabilities and limitations

NA Malarich, GB Rieker - Journal of Quantitative Spectroscopy and …, 2021 - Elsevier
Absorption spectroscopy is traditionally used to determine the average gas temperature and
species concentration along the laser line-of-sight by measuring the magnitude of two or …

Flow field and hot streak migration through a high pressure cooled vanes with representative lean burn combustor outflow

T Bacci, T Lenzi, A Picchi… - … of Engineering for …, 2019 - asmedigitalcollection.asme.org
Modern lean burn aero-engine combustors make use of relevant swirl degrees for flame
stabilization. Moreover, important temperature distortions are generated, in tangential and …

[HTML][HTML] The influence of combustor swirl on pressure losses and the propagation of coolant flows at the Large Scale Turbine Rig (LSTR): Experimental and numerical …

H Werschnik, M Schneider, J Herrmann… - International Journal of …, 2017 - mdpi.com
The aerothermal interaction of the combustor exit flow on the first vane row has been
examined at the Large Scale Turbine Rig (LSTR) at Technische Universität Darmstadt …

The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part I: Change in Expansion Ratio

A Notaristefano, P Gaetani - Journal of …, 2023 - asmedigitalcollection.asme.org
Aeroengine lean-burn combustors release vorticity and temperature perturbations that,
interacting with the first turbine stage, impact the stage aerodynamics, the blade cooling, and …

Study on coupling characteristics between multi-swirler array combustor and NGVs

H Li, J Zhang, G Xie, Y Lou, Z Zhou - Applied Thermal Engineering, 2023 - Elsevier
A novel lean-burn burner effectively reduces NOx emissions from gas turbines, but residual
swirl flow affects the NGV's performance. The multi-point array LDI combustor, as one type of …

Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors

A Andreini, T Bacci, M Insinna, L Mazzei… - Aerospace Science and …, 2018 - Elsevier
The accurate prediction of the fluid dynamic conditions at the exit of gas turbine combustors
are of paramount importance in the aero-thermal design of the aero-engine. In fact, both the …