• 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