Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5.
[Part] I,
, Velocity-diagram study /
by James W. Miser and Warner L. Stewart.

Description

Main Author

Miser, James W.

Related Names

Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1956.

Subjects

Aerodynamics, Transonic.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Blades.

Note

"October 22, 1956."

Physical Description

25 p. : ill. ; 27 cm.

Locate a Print Version

Find in a library

Viewability