Tytuł artykułu
Autorzy
Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Konferencja
International Symposium on Compressor and Turbine Flow Systems - Theory and Application Areas "SYMKOM" (10 ; 26-28.10.2011 ; Łódź, Polska)
Języki publikacji
Abstrakty
This study presents results of tests on the structure of gas flow through a compressing stage of a radial blower. The tests conducted used LDA laser anemometer enabling measurement of velocities in diversified geometries such as, among others, geometries of the compressor rotors. The presented measurement results relate to a half-open axial and radial rotor, for which velocity field s were obtained in two control cross-sections, i.e. in the inlet cross-section and outlet cross-section. The obtained results enabled an evaluation of the effectiveness of the adopted design solutions.
Słowa kluczowe
Rocznik
Tom
Strony
73--82
Opis fizyczny
Bibliogr. 5 poz.
Twórcy
autor
- Poznan University of Technology, Chair of Thermal Engineering, mateusz.grzelczak@put.poznan.pl
Bibliografia
- [1] Eckardt D., Detailed Flow Investigation With in a High - Velocity Centrifugal Compressor Impeller, Trans. of the ASME, J. of Fluids Eng. 1976, Vol. 98, pp. 390-402.
- [2] Eisenlohr G., Krain H., Richter FA, Tiede V., Investigations of the flow through a high pressure Ratio Centrifugal Impeller, ASME, GT -2002-30394, 2002.
- [3] Higashimori H., Hasagawa K., Sumida K., Suita T., Detailed Flow Study of Mach Number 1.6 High Transonic Flow With a Shock Wave in a Pressure Ratio 11 Centrifugal Compressor Impeller, ASME 2004-GT-53435, 2004.
- [4] Japikse D., Centrifugal Compressor Design and Performance, Berlin, Germany September 24-28, 1990, pp. 2, 4-16.
- [5] Krain H., Karpinski G., Beversdorff M., Flow Analysis in a Transonic Centrifugal Compressor Rotor Using 3-component laser Velocimetry, ASME 2001-GT-315, 2001.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-LOD9-0028-0015