Heat transfer characteristic of an impingement cooling system with different nozzle geometry
K Marzec, A Kucaba-Pietal - Journal of Physics: Conference …, 2014 - iopscience.iop.org
The influence of different geometries of the nozzles of an impingement cooling array of six
jets directed to the flat surface on the flow mechanism and the heat transfer were …
jets directed to the flat surface on the flow mechanism and the heat transfer were …
Influence of jet position on local heat transfer distribution under an array of impinging nozzles with non-planar contour of the cooled surface
K Marzec - Heat Transfer Engineering, 2021 - Taylor & Francis
Many experimental and numerical investigations of arrays of impingement cooling jets have
been performed. A lot of them have addressed the problem of cooling with jets directed …
been performed. A lot of them have addressed the problem of cooling with jets directed …
[PDF][PDF] Numerical investigation of local heat transfer distribution on surfaces with a non-uniform temperature under an array of impinging jets with various nozzle …
K Marzec, A Kucaba-Piętal - Journal of …, 2017 - warminski.pollub.plwww.ptmts.org.pl
Numerical calculations of heat transfer characteristics of an impingement cooling system
with a non-uniform temperature on a cooled surface using ANSYS CFX have been …
with a non-uniform temperature on a cooled surface using ANSYS CFX have been …
Numerical investigation of a heat transfer characteristics of an impingement cooling system with non-uniform temperature on a cooled surface
K Marzec, A Kucaba-Pietal - Journal of Physics: Conference …, 2016 - iopscience.iop.org
A series of numerical analysis have been performed to investigate heat transfer
characteristics of an impingement cooling array of ten jets directed to the flat surface with …
characteristics of an impingement cooling array of ten jets directed to the flat surface with …
Enhancement of heat transfer performance on nacelle lip-skin for swirl anti-icing
MA Ismail - 2014 - eprints.kingston.ac.uk
Ice accretion on the wing and nacelle leading edges diminishes aerodynamic performance
and increases fuel consumption and chances of aircraft crash. For these reasons, the …
and increases fuel consumption and chances of aircraft crash. For these reasons, the …