Box 1
Container
Contains 1 Result:
Aerodynamic Design of a Variable Mach Number Supersonic Nozzle for the ABMA 14 x 14 Inch Wind Tunnel, 1957-04-23
File — Box: 1, Folder: 3
Content Description
From the Collection:
This collection includes materials on wind tunnel research at NASA, Chrysler, and Thiokol, as well as journal articles written by the donor on various technical topics.
Dates:
1957-04-23