The U.S. Naval Ordnance Laboratory Hypersonic Tunnel
Description:
This report describes the aerodynamic capability and physical plant installation of the U.S. Naval Ordnance Laboratory's Hypersonic Tunnel. The tunnel is a high pressure blowdown facility, using air as the working gas, operating at Mach numbers 5, 6, 7, 8, 9 and 10 with test section Reynolds Number from 3000 thousand to 50 million per foot (Author). The air supply system, air heating plant, exhaust system and other features are described in the report along with schematic diagrams, photographs,…
more
Date:
April 12, 1967
Creator:
Geineder, F.; Schlesinger, M. I.; Baum, G. & Cornett, R.
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department