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The effects of lean and sweep on transonic fan performance a computational study

Autorzy
Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Konferencja
Seminar/summer school on "CFD for turbomachinery applications" (01-03.09.2001, Gdańsk, Poland)
Języki publikacji
EN
Abstrakty
EN
The aerodynamics of transonic fans is discussed with emphasis on the use of three-dimensional design techniques, such as blade sweep and lean, to improve their performance. In order to study the interaction of these 3D features with the shock pattern a series of five different designs is produced and analysed by CFD. It is found that the 3D features have remarkably little effect on the shock pattern near the tip where the shock must remain perpendicular to the casing. Lower down the blade significant shock sweep, and hence reduced shock loss, can be induced by 3D design but this is usually at the expense of reduced stall margin and increased loss elsewhere along the blade span. Overall, very little change in efficiency is produced by blade sweep or lean. However, forwards lean of the rotor does produce a small increase in mass flow. Radial migration of the boundary fluid on the suction surface behind the shock is shown to play a large part in the aerodynamics near the blade tip.
Rocznik
Strony
7--23
Opis fizyczny
Bibliogr. 7 poz., rys.
Twórcy
autor
  • Cambridge University Engineering Department, Madingley Road, Cambridge, CB3ODY UK
Bibliografia
  • [1] Calvert W J and Ginder R B 1999 Proc. Instn. Mech. Engrs., Part C, J. Mech. Eng. Sci. 213 (5) 419
  • [2] Denton J D 1996 Proc. 3rd International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, Beijing, China, pp. 3-14
  • [3] Neubert R J, Hobbs D E and Weingold H D 1990 ,47,4,4 Paper 90-1915
  • [4] Denton J D 1993 ASME J. Turbomachinery 115 (4) 621
  • [5] Wadia A R, Szucs P N and Crall D W 1997 ASME Paper 97-GT-401
  • [6] Denton J D 1994 AGARD LS 195, Turbomachinery design using CFD, Lecture 3, pp. 1-14
  • [7] Denton J D and Xu L 1999 Proc. Instn. Mech. Engrs., Part C, J. Mech. Eng. Sci. 213 (2) 125.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BAT3-0010-0063
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