Magnetic Suspension and Balance System for Wind Tunnel Application-Reference-Cited by-同舟云学术

Magnetic Suspension and Balance System for Wind Tunnel Application

Published:1963-11 Issue:635 Volume:67 Page:717-724
ISSN:0368-3931
Container-title:The Journal of the Royal Aeronautical Society
language:en
Short-container-title:J. R. Aeronaut. Soc.

Author:

Chrisinger J. E.,Tilton E. L.,Parkin W. J.,Coffin J. B.,Covert E. E.

Abstract

SummaryIn this article a magnetic suspension and balance system suitable for wind tunnel application is discussed. General considerations are presented that illustrate the nature of the problems to be solved as well as one solution of these problems.Finally some initial wind tunnel data are presented.

Publisher

Cambridge University Press (CUP)

Reference7 articles.

1. Chrisinger J. et al. The Design and Initial Operation of a Magnetic Model Suspension and Force Measurement System. Aeronautical Research Laboratories, Office of Aerospace Re search, U.S. Air Force Report ARL 63-16.

2. Suspension Magnetique I'ane Maquette en Soufflerie;Tournier;La Recherche Aeronautique,1957

3. Private Communications.

4. Beams J. W. Magnetic Suspension Ultracentrifuge Circuits. Electronics, March 1954.

5. Kuhlthau A. R. The Investigation of Low Density Drag Phenomena Utilizing Laboratory Techniques. Paper No. 29, Proceedings of the Fourth U.S. Navy Symposium on Aero- ballistics, Nav. Ord. Report No. 5904, 1st May 1958.

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