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Numerical Investigation of Airfoil Clocking in a Three-Stage Low Pressure Turbine

[+] Author Affiliations
Andrea Arnone, Michele Marconcini, Roberto Pacciani

University of Florence, Firenze, Italy

Claudia Schipani, Ennio Spano

Fiat Avio S.p.A., Torino, Italy

Paper No. 2001-GT-0303, pp. V001T03A008; 9 pages
doi:10.1115/2001-GT-0303
From:
  • ASME Turbo Expo 2001: Power for Land, Sea, and Air
  • Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
  • New Orleans, Louisiana, USA, June 4–7, 2001
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7850-7
  • Copyright © 2001 by ASME

abstract

A quasi–three–dimensional, blade–to–blade, time–accurate, viscous solver w as used for a three–stage LP turbine study Due to the low Reynolds number, transitional computations were performed. Unsteady analyses were then carried out by varying the circumferential relative position of consecutive vanes and blade rows to study the effects of clocking on the turbine’s performance. A clocking strategy developed in order to limit the number of configurations to be analyzed is discussed. The optimum analytically–determined clocking position is illustrated for two different operating conditions, referred to as cruise and takeoff.

The effects of clocking on wake interaction mechanisms and unsteady blade loadings is presented and discussed. For low Reynolds number turbine flows, the importance of taking transition into account in clocking analysis is demonstrated by a comparison with a fully turbulent approach.

Copyright © 2001 by ASME
Topics: Pressure , Turbines , Airfoils

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