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Experimental feasibility study of the application of magnetic suspension techniques to large-scale aerodynamic test facilitiesBased on the premises that (1) magnetic suspension techniques can play a useful role in large-scale aerodynamic testing and (2) superconductor technology offers the only practical hope for building large-scale magnetic suspensions, an all-superconductor three-component magnetic suspension and balance facility was built as a prototype and was tested successfully. Quantitative extrapolations of design and performance characteristics of this prototype system to larger systems compatible with existing and planned high Reynolds number facilities have been made and show that this experimental technique should be particularly attractive when used in conjunction with large cryogenic wind tunnels.
Document ID
19740052633
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zapata, R. N.
Humphris, R. R.
Henderson, K. C.
(Virginia, University Charlottesville, Va., United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1974
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER 74-615
Meeting Information
Meeting: Aerodynamic Testing Conference
Location: Bethesda, MD
Start Date: July 8, 1974
End Date: July 10, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A35383
Funding Number(s)
CONTRACT_GRANT: NGR-47-005-112
CONTRACT_GRANT: NGR-47-005-110
CONTRACT_GRANT: NGR-47-005-029
CONTRACT_GRANT: NSG-1010
Distribution Limits
Public
Copyright
Other

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