DocumentCode
1150544
Title
Thermal stresses in an actively cooled two-piece rail structure
Author
Satapathy, S. ; Persad, C.
Author_Institution
Inst. for Adv. Technol., Univ. of Texas, Austin, TX, USA
Volume
39
Issue
1
fYear
2003
Firstpage
468
Lastpage
471
Abstract
In this paper, we evaluate the thermal stress arising in rails and supporting structures of an electromagnetic launcher. We examine the effects of using rail overlays and active cooling. These not only reduce the peak temperature, but also affect the overall thermal gradient. The transverse temperature distribution within the rail structure is obtained by a numerical solution of magnetic and thermal diffusion equations. The effects of cooling rate and cooling channel location on the temperature distribution are evaluated. The resultant thermal stress in the rail structure is then computed. The analysis yields two fruitful approaches: use of thin resistive overlays, which minimize thermal stress on the structure by effecting a more even temperature distribution; and use of active cooling at a central location, which even though ineffective at very early times, enables more efficient heat removal in the time between launches.
Keywords
claddings; cooling; electromagnetic launchers; stress analysis; temperature distribution; thermal analysis; thermal diffusion; thermal stresses; actively cooled two-piece rail structure; conductor cooling; cooling channel location; cooling rate; efficient heat removal; electromagnetic launcher; magnetic diffusion equations; numerical solution; rail life; rail overlays; resistive cladding; supporting structures; thermal diffusion equations; thermal gradient; thermal stress; thin resistive overlays; transverse temperature distribution; Conductors; Cooling; Electromagnetic launching; Fatigue; Government; Rails; Temperature distribution; Thermal factors; Thermal resistance; Thermal stresses;
fLanguage
English
Journal_Title
Magnetics, IEEE Transactions on
Publisher
ieee
ISSN
0018-9464
Type
jour
DOI
10.1109/TMAG.2002.806385
Filename
1179868
Link To Document