Oxide-dispersion-strengthened turbine blades
Subtitle: materials for advanced turbine engines, project completion report, project 4
By: by P.P. Millan, Jr. ... [et al.].
Contributors: Millan, P. P.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-179561.
Publisher: Garrett Turbine Engine Co.; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1987
Place of publication: [Phoenix, Ariz.]; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Alloys.; Engine tests.; Feasibility analysis.; Gas turbines.; High temperature.; Oxide dispersion strengthening.; Turbine blades.
Other titles: Oxide dispersion strengthened turbine blades.
Notes: Distributed to depository libraries in microfiche.

Description based on v. 2.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 1 microfiche.