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Numerical simulation and modification of 3D flow phenomena in an axial flow fan

Autorzy
Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This work aims to study and analyze the behavior of flow in an axial flow fan using numerical simulation based on solving Reynolds-averaged Navier-Stokes equations coupled with a modified Spalart-Allaras turbulence model. In the present work, different flow phenomena occuring in an axial flow fan were presented and interpreted at different design conditions and at different regions, with special concern to the rotor exit and stator regions. Large vortices and reverse flow at the stator suction side were observed under high loading conditions. These are mainly due to radial and centrifugal effects in the fluid due to a decreasing flow rate. To avoid this type of flow, the stator flow pattern has been modified using a new stator blade. This blade was designed by changing the stator stagger angle by 10o in the radial direction. This study indicates that the flow in the modified stator region behaves well and gives better performance than that obtained when using a baseline stator, especially under high loading conditions. This study also indicates that the stator stagger angle has a significant effect on modifying the fan performance.
Słowa kluczowe
Rocznik
Strony
199--213
Opis fizyczny
Bibliogr. 14 poz., rys., tab.
Twórcy
autor
  • School of Energy and Power Engineering, Huazhong University of Science and Technology, Wuhan, 430074, P. R., China
autor
  • School of Energy and Power Engineering, Huazhong University of Science and Technology, Wuhan, 430074, P. R., China
  • School of Energy and Power Engineering, Huazhong University of Science and Technology, Wuhan, 430074, P. R. China, mohandei@yahoo.com
Bibliografia
  • [1] Denton J D and Dawes W N 1999 J. Mech. Engng. Sci.C 213(C2) 107
  • [2] Tallman J A 1999 Simulation of Tip Leakage Flows in a Turbine Rotor using ComputationalFluid Dynamics, MSc Thesis in Mechanical Engineering, Pennsylvania State University
  • [3] Jens F, Sven B, Gunter K and Udo S 2001 ASME J. Turbomachinery123483
  • [4] Keqi W and Inoure M 1984 China-Japan Joint Conf. Hydraulic Machinery and Equipment,Hangzhou, China, pp. 21–30
  • [5] Elhadi E E, Lie X and Keqi W 2002 4thInt. Conf. Pumps and Fans, Tsinghua University,Beijing, pp. 327–333
  • [6] Chunill H, FuLin T and James L 1998 JSME Int. J., Series B41(1) 200
  • [7] Dalcles J and Zilliac G G 1995AIAA J.33(9) 1561
  • [8] Spalart P and Allmaras S 1992 Technical Report, American Institute of Aeronautics and Astronautics, AIAA-92-0439
  • [9] Pantankar S V 1972 Int. J. Heat and Mass Transfer151787
  • [10] Pantankar S V 1980 Numerical Heat Transfer and Fluid Flow, MC Graw-Hill
  • [11] Ruprecht A and Bauer C 1999 ASME PVP Conference, CFD Symposium, Boston,www.ihs.uni-stuttgart.de/forschung/veroeff/stroem/v199901.pdf
  • [12] Sbardella L and Imregun M 2001 ASME, J. Turbomachinerybf 123 568
  • [13] Yamamoto A and Nouse H 1988 Effects of Incidence on Three Dimensional Flow in a LinearTurbine Cascade, ASME88-GT-110
  • [14] Sabesky R H, Acosta A J and Hauptmann H 1971 Fluid Flow, 2ndEdition, New York,Macmillan
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BAT3-0010-0020
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