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The MIT Blowdown Turbine Facility FREE

[+] Author Affiliations
A. H. Epstein, G. R. Guenette

Massachusetts Institute of Technology, Cambridge, MA

R. J. G. Norton

Rolls-Royce Inc., Atlanta, GA

Paper No. 84-GT-116, pp. V004T09A011; 9 pages
doi:10.1115/84-GT-116
From:
  • ASME 1984 International Gas Turbine Conference and Exhibit
  • Volume 4: Heat Transfer; Electric Power
  • Amsterdam, The Netherlands, June 4–7, 1984
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7949-8
  • Copyright © 1984 by ASME

abstract

A short duration (0.4 sec) test facility, capable of testing 0.5-meter diameter, film-cooled, high work aircraft turbine stages at rigorously simulated engine conditions has been designed, constructed, and tested. The simulation capability of the facility extends up to 40 atm inlet pressure at 2500°K (4000°F) turbine inlet temperatures. The facility is intended primarily for the exploration of unsteady, three-dimensional fluid mechanics and heat transfer in modern turbine stages.

Copyright © 1984 by ASME
Topics: Turbines
This article is only available in the PDF format.

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