Materials for advanced turbine engines (MATE) project 3 design, fabrication and evaluation of an oxide dispersion strengthened sheet alloy combustor liner.
By: S. Bose and K.D. Sheffler.
Contributors: Sheffler, Keith D.; United States. National Aeronautics and Space Administration.
Series: NASA CR -- 180892.; NASA contractor report -- NASA CR-180892.
Publisher: National Aeronautics and Space Administration
Published: 1990
Place of publication: [Washington, DC
Language: eng
Format: Microform
Subjects: Aircraft gas-turbines -- Combustion chambers.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1990. 1 microfiche.