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Some aspects of wind tunnel magnetic suspension systems with special application at large physical scales

Some aspects of wind tunnel magnetic suspension systems with special application at large physical scales
Some aspects of wind tunnel magnetic suspension systems with special application at large physical scales
Despite over a quarter of a century of development, wind tunnel magnetic suspension and balance systems (MSBSs) have so far failed to find application at the large physical scales necessary for the majority of whole model aerodynamic testing. Recent developments, such as the cryogenic operation of wind tunnels and advances in superconducting electromagnet technology have greatly reduced the apparent cost of a large, or perhaps more specifically, high Reynolds Number MSBS (LMSBS). Many difficulties remain, however, and three are addressed in this thesis.
A powerful method of magnetic roll torque generation is essential for any LMSBS. Two variants of the new Spanwise Magnet scheme are studied herein. Spanwise Permanent Magnets are shown to be a practical method and are experimentally demonstrated using the Southampton University MSBS, though precise evaluation of maximum torque capabilities has not been possible.
Extensive computations of the performance of the Spanwise Iron Magnet scheme indicate potentially powerful capability, limited principally by current electromagnet technology. Some experimental verification of the computed performance at low applied field levels is presented.
Aerodynamic testing at extreme attitudes is shown to be practical in relatively conventionally configured MSBSs. Preliminary operation of the Southampton University MSBS over a wide range of angles of attack is demonstrated.
The impact of a requirement for highly reliable operation on the overall architecture of LMSBSs is studied. It is shown that the system’s cost and complexity need not be unduly increased, provided certain of its unique characteristics are exploited.
University of Southampton
Britcher, Colin Paul
0d1705b2-b988-4d4c-b373-c4d37fd2aaca
Britcher, Colin Paul
0d1705b2-b988-4d4c-b373-c4d37fd2aaca
Goodyer, M.J.
262e49a1-2b80-42d5-877d-9e8963f9e543

Britcher, Colin Paul (1982) Some aspects of wind tunnel magnetic suspension systems with special application at large physical scales. University of Southampton, Department of Aeronautics and Astronautics, Doctoral Thesis, 332pp.

Record type: Thesis (Doctoral)

Abstract

Despite over a quarter of a century of development, wind tunnel magnetic suspension and balance systems (MSBSs) have so far failed to find application at the large physical scales necessary for the majority of whole model aerodynamic testing. Recent developments, such as the cryogenic operation of wind tunnels and advances in superconducting electromagnet technology have greatly reduced the apparent cost of a large, or perhaps more specifically, high Reynolds Number MSBS (LMSBS). Many difficulties remain, however, and three are addressed in this thesis.
A powerful method of magnetic roll torque generation is essential for any LMSBS. Two variants of the new Spanwise Magnet scheme are studied herein. Spanwise Permanent Magnets are shown to be a practical method and are experimentally demonstrated using the Southampton University MSBS, though precise evaluation of maximum torque capabilities has not been possible.
Extensive computations of the performance of the Spanwise Iron Magnet scheme indicate potentially powerful capability, limited principally by current electromagnet technology. Some experimental verification of the computed performance at low applied field levels is presented.
Aerodynamic testing at extreme attitudes is shown to be practical in relatively conventionally configured MSBSs. Preliminary operation of the Southampton University MSBS over a wide range of angles of attack is demonstrated.
The impact of a requirement for highly reliable operation on the overall architecture of LMSBSs is studied. It is shown that the system’s cost and complexity need not be unduly increased, provided certain of its unique characteristics are exploited.

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Published date: July 1982
Organisations: University of Southampton, Aerodynamics & Flight Mechanics

Identifiers

Local EPrints ID: 52333
URI: http://eprints.soton.ac.uk/id/eprint/52333
PURE UUID: 101d617d-6a7c-4c3c-9266-fe30d3f9ddfb

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Date deposited: 27 Aug 2008
Last modified: 15 Mar 2024 10:33

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Contributors

Author: Colin Paul Britcher
Thesis advisor: M.J. Goodyer

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