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A preliminary investigation of the dynamic force-calibration of a magnetic suspension and balance systemThe aerodynamic forces and moments acting upon a magnetically suspended wind tunnel model are derived from calibrations of suspension electro magnet currents against known forces. As an alternative to the conventional calibration method of applying steady forces to the model, early experiences with dynamic calibration are outlined, that is a calibration obtained by oscillating a model in suspension and deriving a force/current relationship from its inertia force and the unsteady components of currents. Advantages of dynamic calibration are speed and simplicity. The two methods of calibration applied to one force component show good agreement.
Document ID
19850015497
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Goodyer, M. J.
(Southampton Univ.)
Date Acquired
September 5, 2013
Publication Date
May 1, 1985
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-172580
NAS 1.26:172580
Report Number: NASA-CR-172580
Report Number: NAS 1.26:172580
Accession Number
85N23808
Funding Number(s)
CONTRACT_GRANT: NSG-7523
PROJECT: RTOP 505-31-53
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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