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pro vyhledávání: '"C. Golia"'
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Publikováno v:
Progress in Aerospace Sciences. 34:257-345
This paper reviews experimental and computational methods used for simulation of ice accretion on aircraft flying through icing conditions. Such methods were recently reviewed by the AGARD FDP Working Group 20 and the present paper represents a revis
Publikováno v:
Acta Astronautica. 41:113-120
Thermocapillary flow arises under zero-gravity in a plane layer of liquid metal bounded by two plane fixed interfaces with a passive gas and held by two differentially heated walls. On the interfaces the surface tension depends quadratically, with a
Publikováno v:
Acta Astronautica. 38:193-208
The aim of this paper is to advance the numerical investigation of unsteady thermocapillary migration of gas bubbles in a fully confined non-isothermal liquid. The relevance of the study is twofold: to support space experiments such as the Italian ex
Publikováno v:
Advances in Space Research. 13:133-140
In recent theoretical developments, non-linear irreversible thermodynamic effects, like Burnett stresses and slip boundary conditions, have been recognized as playing an important role under typical conditions encountered during vapour crystal growth
Autor:
A. Viviani, C. Golia
Publikováno v:
Advances in Space Research. 13:87-96
This paper deals with thermal Marangoni and natural convection in two superposed immiscible liquids enclosed in a rectangular cavity with differentially heated end walls. The problem is solved via a two-dimensional, unsteady, finite difference numeri
Autor:
C. Golia, B. Buonomo
Publikováno v:
WIT Transactions on Modelling and Simulation, Vol 46.
We explore novel ideas to improve the accuracy of the integral approximation of differential operators (Gradient and Laplacian) in the simulation of thermal viscous problems with Lagrangian Blob mesh-less methods. Basically we investigate and develop
Autor:
Luciano Blasi, Alessandro Soprano, Francesco Caputo, F. Scaramuzzino, Alberto D'Amore, Luigi Iuspa, C. Golia, Luigi Grassia
The behavior of the wing of an aircraft is characterized by the complex interaction among dynamic (distribution of the masses), elastic (ownership of the materials) and aerodynamic (shapes, forces and moments) phenomena. As a rule it is expected from
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e32c62b589c79ff196fb9a31347ae62d
http://hdl.handle.net/11591/205758
http://hdl.handle.net/11591/205758
Akademický článek
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