Design of the MIT Breakdown Turbine Facility
Name
16206191.pdf
Size
6.05 MB
Format
Adobe PDF
Checksum (MD5)
0214fc7e105fa395e6367452d3d5c60a
Author(s)
Epstein, Alan H. (Alan Henry)
Guenette, Gerald R. (Gerald Roger)
Norton, Robert J. G.
Alternative Title
Design of the Massachusetts Institute of Technology Breakdown Turbine Facility
Date Issued
1985
Publisher
Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1985]
Series/Report no.
GTL report #183
Abstract
Summary: This report details the design, construction, and preliminary testing of a short duration (0.4 sec) test facility capable of testing 0.5 meter diameter, film cooled, high work aircraft turbine stages under conditions which rigorously simulate actual engine conditions. The simulation capability of the facility extends up to 40 atm inlet pressure at 2500 0K (40000F) turbine inlet temperatures. The facility is intended primarily for the exploration of unsteady, three-dimensional fluid mechanics and heat transfer in modern turbine stages.
Description
April 1985
Includes bibliographical references (page 151)
Persistent DSpace Link
