Experimental investigation of an air-cooled turbine operating in a turbojet engine at turbine inlet temperatures up to 2500 degrees F /
by Reeves P. Cochran and Robert P. Dengler.

Description

Main Author: Cochran, Reeves P.
Related Names: Dengler, Robert P.
United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration : [1961]
Subjects: Propulsion systems, air-jet.
Propulsion system elements.
Note: Cover title.
"July 1961."
Propulsion system elements; Propulsion systems, air-jet.
Physical Description: 47 p. : ill. ; 26 cm.
Locate a Print Version: Find in a library

Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign