Performance and operating characteristics of the arc-driven langley 6-inch shock tube
1972
27 S
Ill
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
The NASA-Langley 20-inch supersonic wind tunnel
AIAA | 1986
|The Langley 15-inch Mach 6 High Temperature Tunnel
AIAA | 1992
|