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Wyszukujesz frazę "perforated wall" wg kryterium: Temat


Wyświetlanie 1-2 z 2
Tytuł:
Hole extension effect on transpiration flow efficiency
Autorzy:
Lewandowski, T.
Doerffer, P.
Powiązania:
https://bibliotekanauki.pl/articles/1938639.pdf
Data publikacji:
2015
Wydawca:
Politechnika Gdańska
Tematy:
perforated wall
L/D ratio
mass flow rate
efficiency
Opis:
The present analysis of the hole extension effect on the transpiration flow efficiency is a part of the research [1] which aims at defining a physical transpiration model of the flow through perforated plates. Perforated walls find a wide use as a method of flow control and effusive cooling. Some data on the L/D (hole length to diameter ratio) effect on the flow structure and mass flow rate may be found in the literature [2, 3], but all those works concern holes of a diameter at least one order of magnitude larger than those used in the simulations presented in this paper. Due to the size of the analyzed holes and their cylindrical shape, the only method of analysing the flow through such holes is the numerical method. In the conducted simulations, the holes were D = 0.6 mm, 0.3 mm and 0.125 mm in diameter and the perforation values were equal to 4%, 5%, 8% and 10%. The L/D ratio was changed between 0.25 and 8. The data bank of the flow through the cylindrical holes was produced. The hole extension has a significant influence on the obtained mass flow rate and, consequently, on the transpiration flow efficiency. In addition, entrance effects appear to be important.
Źródło:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk; 2015, 19, 2; 121-128
1428-6394
Pojawia się w:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Passive control of shock wave applied to helicopter rotor high-speed impulsive noise reduction
Autorzy:
Doerffer, P.
Szulc, O.
Powiązania:
https://bibliotekanauki.pl/articles/1943208.pdf
Data publikacji:
2010
Wydawca:
Politechnika Gdańska
Tematy:
shock wave
passive control
perforated wall
transpiration
helicopter rotor in hover
high-speed impulsive noise
Opis:
A strong, normal shock wave, terminating a local supersonic area on an airfoil (or a helicopter blade), not only limits the aerodynamic performance, but also becomes a source of High-Speed Impulsive (HSI) noise. The application of a passive control system (a cavity covered by a perforated plate) on a rotor blade should reduce the noise created by the moving shock. This article describes numerical investigations focused on the application of a passive control device on a helicopter blade in high-speed transonic hover conditions to weaken the shock wave – the main source of HSI noise.
Źródło:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk; 2010, 14, 3; 297-305
1428-6394
Pojawia się w:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk
Dostawca treści:
Biblioteka Nauki
Artykuł
    Wyświetlanie 1-2 z 2

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