Title :
Hypervelocity wind tunnel 9 control system
Author :
Newell, Douglas F. ; Rinaldi, Stephen F.
Author_Institution :
US Naval Surface Warfare Center, Silver Spring, MD, USA
Abstract :
The US Naval Surface Warfare Center Hypervelocity Wind Tunnel 9 operates from Mach 8 to Mach 14 with Reynolds numbers ranging from 75,000 per foot to 53,000,000 per foot. The Tunnel 9 facility control system was recently modernized. The architecture of the original and upgraded control system is described. In the upgraded system programmable logic controllers provide safety interlocking and input/output interfacing to the facility valve system. Mini computers (MicroVax II) provide an operator interface to the logic controllers, the sensors, the prerun initialization and online tunnel run command and status monitors, the displays, and tunnel condition data acquisition
Keywords :
aerospace computing; computerised control; computerised instrumentation; flow control; programmable controllers; programmed control; valves; wind tunnels; (MicroVax II; Mach 8 to Mach 14; PCL; command and status monitors; data acquisition; displays; input/output interfacing; maintenance; offline system; online control; operator interface; prerun initialization; programmable logic controllers; safety interlocking; sensors; software; valve; Computer architecture; Computer displays; Computer interfaces; Control systems; Data acquisition; Foot; Logic; Programmable control; Safety; Valves;
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1991. ICIASF '91 Record., International Congress on
Conference_Location :
Rockville, MD
DOI :
10.1109/ICIASF.1991.186260
