Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel
By: A. K. Sreekanth.
Publisher: Dept. of Aeronautical Engineering and Aerophysics
Published: 1956
Place of publication: [Downsview, Ont.]
Number of pages: 25
Subjects: Low density wind tunnels; Wind tunnel nozzles
Notes: Thesis (M.A.Sc.) - University of Toronto, 1956.

Includes bibliographical references.