DocumentCode :
2950333
Title :
External 6-component wind tunnel balances for aerospace simulation facilities
Author :
Preusser, Timm ; Polansky, Lubomir
Author_Institution :
Carl Schenck AG, Darmstadt, West Germany
fYear :
1989
fDate :
18-21 Sep 1989
Firstpage :
488
Lastpage :
495
Abstract :
The measurement function of wind tunnel balances is to separate vectorially the force vector K into the three X-Y-Z coordinate force directions or moments. The state of the art for external balances is strain-gage platform balances with computer separation of forces and moments. On the basis of experience gained with such balances, a new type of balance has been developed which combines the advantages of computer separation with the advantages of both platform- and pyramidal-type balances. This allows for a significant reduction of the load cells required for calibration of different heights within the test section and for considerable improvement of measurement accuracy of roll, pitch, and yaw moments
Keywords :
aerospace simulation; balances; computerised instrumentation; force measurement; strain gauges; wind tunnels; 6-component wind tunnel balances; X-Y-Z coordinate force directions; aerospace simulation facilities; computer; external balances; force vector K; pitch; pyramidal-type balances; strain-gage platform balances; yaw moments; Aerodynamics; Aerospace simulation; Capacitive sensors; Coordinate measuring machines; Electric variables measurement; Force measurement; Frequency measurement; Interference; Mechanical variables measurement; 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.1989.77704
Filename :
77704
Link To Document :
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