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