DocumentCode
2941896
Title
A new data acquisition, display and control system for the ARA transonic wind tunnel
Author
Coulton, David G.
fYear
1989
fDate
18-21 Sep 1989
Firstpage
38
Lastpage
49
Abstract
A new data acquisition system has been designed and manufactured by the Systems Department of the Aircraft Research Association (ARA) Ltd. for use in their transonic wind tunnel at Bedford, England. This system is based on a Radstone single-board computer utilizing a Motorola 68020 processor operating on a VME bus. The calibration system, which is referable back to national standards, supplemented by a precision bridge circuit, constantly assures the user of the quality of data being recorded. The authors highlight the development of data logging at ARA and consider the system requirements and specifications. The most important constituent parts of the system are described, as are several planned enhancements
Keywords
calibration; computerised control; computerised instrumentation; data acquisition; transonic flow; wind tunnels; ARA transonic wind tunnel; Aircraft Research Association; Motorola 68020 processor; Radstone single-board computer; VME bus; bridge circuit; calibration; computerised instrumentation; control; data acquisition; data logging; display; national standards; Aircraft manufacture; Color; Computer aided manufacturing; Computer interfaces; Control systems; Data acquisition; Displays; Force measurement; Pressure measurement; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 1989. ICIASF '89 Record., International Congress on
Conference_Location
Gottingen
Type
conf
DOI
10.1109/ICIASF.1989.77657
Filename
77657
Link To Document