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An investigation into force-moment calibration techniques applicable to a magnetic suspension and balance systemThe problem of determining the forces and moments acting on a wind tunnel model suspended in a Magnetic Suspension and Balance System is addressed. Two calibration methods were investigated for three types of model cores, i.e., Alnico, Samarium-Cobalt, and a superconducting solenoid. Both methods involve calibrating the currents in the electromagnetic array against known forces and moments. The first is a static calibration method using calibration weights and a system of pulleys. The other method, dynamic calibration, involves oscillating the model and using its inertia to provide calibration forces and moments. Static calibration data, found to produce the most reliable results, is presented for three degrees of freedom at 0, 15, and -10 deg angle of attack. Theoretical calculations are hampered by the inability to represent iron-cored electromagnets. Dynamic calibrations, despite being quicker and easier to perform, are not as accurate as static calibrations. Data for dynamic calibrations at 0 and 15 deg is compared with the relevant static data acquired. Distortion of oscillation traces is cited as a major source of error in dynamic calibrations.
Document ID
19890000690
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Eskins, Jonathan
(Southampton Univ.)
Date Acquired
September 5, 2013
Publication Date
August 1, 1988
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-181695
NAS 1.26:181695
AASU-88/4
Report Number: NASA-CR-181695
Report Number: NAS 1.26:181695
Report Number: AASU-88/4
Accession Number
89N10061
Funding Number(s)
PROJECT: RTOP 505-61-01-02
CONTRACT_GRANT: NSG-7523
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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