Analysis of metal temperature and coolant flow with a thermal-barrier coating on a full-coverage-film-cooled turbine vane
By: Peter L. Meitner, Propulsion Laboratory, AVRADCOM Research and Technology Laboratories, Lewis Research Center
Contributors: United States. Army Research and Technology Laboratories. Propulsion Laboratory; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper ; 1310; AVRADCOM technical report ; 78-20
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Subjects: Heat -- Transmission; Turbines -- Cooling; Aerodynamic heating
Notes: Aug. 1978

Includes bibliographical references