Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel - Info and Reading Options
By A. K. Sreekanth
"Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel" was published by Dept. of Aeronautical Engineering and Aerophysics in 1956 - [Downsview, Ont.] and it has 25 pages.
“Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel” Metadata:
- Title: ➤ Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel
- Author: A. K. Sreekanth
- Number of Pages: 25
- Publisher: ➤ Dept. of Aeronautical Engineering and Aerophysics
- Publish Date: 1956
- Publish Location: [Downsview, Ont.]
“Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel” Subjects and Themes:
- Subjects: Low density wind tunnels - Wind tunnel nozzles
Edition Specifications:
- Pagination: 25 leaves :
Edition Identifiers:
- The Open Library ID: OL18999688M - OL6053531W
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