DocumentCode :
1174418
Title :
Hotshot Wind Tunnel Force Measurement
Author :
Berry, J. ; Hoarau, R.
Author_Institution :
ONERA, Chatillon-sous-Bagneux, Seine, France
Issue :
1
fYear :
1965
Firstpage :
4
Lastpage :
9
Abstract :
A description is given of an internal balance capable of withstanding tunnel starting loads of the order of twenty times the amplitude of the forces to be measured during brief-duration hotshot tunnel runs. Large starting forces applied as shock loads necessitate inertia compensation to nullify parasitic signals. Quartz sensing elements statically are used. Dynamic response is within one percent of the final value for a duration of three milliseconds. The inertia compensation and compensation coefficient determinations are described. The readout system uses involving analog computation techniques are presented. Typical results are given and the advantages of inertia compensation are described.
Keywords :
Acceleration; Aerodynamics; Aerospace electronics; Analog computers; Cables; Content addressable storage; Electric shock; Force measurement; Frequency; Impedance; Force measurement; hotshot; inertia compensation; internal balance; shock loads; wind tunnel;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1965.4501646
Filename :
4501646
Link To Document :
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