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Improving the Aero-Thermal Characteristics of Turbomachinery Cascades

[+] Author Affiliations
Marcello Manna, Raffaele Tuccillo

Università di Napoli “Federico II”, Napoli, Italy

Paper No. GT2002-30596, pp. 981-993; 13 pages
doi:10.1115/GT2002-30596
From:
  • ASME Turbo Expo 2002: Power for Land, Sea, and Air
  • Volume 5: Turbo Expo 2002, Parts A and B
  • Amsterdam, The Netherlands, June 3–6, 2002
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 0-7918-3610-X | eISBN: 0-7918-3601-0
  • Copyright © 2002 by ASME

abstract

The paper presents the application of an optimization procedure to the aero-thermal design of high performance turbomachinery cascades. The blade profiles are parameterized with fourth order Bezier polynomials for the pressure and suction sides, and quadratic functions for the leading and trailing edges, according to the composite curve approach. Evidence is given that fairly complicated blade shapes are well approximated by the present parameterization. The method is applied to an existing nozzle guide vane for which extensive and detailed experimental data are available, with the objective of decreasing in an integral sense the thermal load, maintaining or increasing the blade efficiency and the aerodynamic load. The results demonstrate that despite the excellence of the initial design, there is room for improvements.

Copyright © 2002 by ASME
Topics: Turbomachinery

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