Two-layer thermal barrier coating for turbine airfoils - furnace and burner rig test results
By: Stephan Stecura ; Lewis Research Center, Cleveland, Ohio.
Contributors: Lewis Research Center.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum ; NASA TM X-3425; NASA technical memorandum -- X-3425.
Publisher: U.S. National Aeronautics and Space Administration; for sale by the National Technical Information Service
Published: 1976
Place of publication: Washington; Springfield, Va
Language: eng
Number of pages: 18
Subjects: Airplanes -- Turbine-propeller engines.; Aircraft gas-turbines.
Notes: Cover title.

Bibliography: p. 10.