scholarly journals Optimization of a Convex Rail Design for Electromagnetic Launchers

2020 ◽  
Vol 48 (6) ◽  
pp. 2266-2273
Author(s):  
Hakan Polat ◽  
Nail Tosun ◽  
Doga Ceylan ◽  
Ozan Keysan
2019 ◽  
Vol 47 (5) ◽  
pp. 2135-2135
Author(s):  
David Wetz ◽  
Xinjie Yu ◽  
Markus Schneider

2016 ◽  
Vol 44 (2) ◽  
pp. 174-177 ◽  
Author(s):  
Zhipeng Lin ◽  
Zhenxiang Liu ◽  
Dong Yang ◽  
Jianming Ouyang ◽  
Lijia Yang

1984 ◽  
Vol 20 (2) ◽  
pp. 200-202 ◽  
Author(s):  
W. Weldon ◽  
H. Woodson

1989 ◽  
Vol 111 (3) ◽  
pp. 326-331
Author(s):  
E. P. Fahrenthold

The relatively recent development of very high-energy density pulsed power supplies has motivated a renewed interest in the structural design of electromagnetic launchers. Cascade design electromagnetic launcher pressure vessels offer convenient maintenance access to high wear rate components of the structure while satisfying an unusual combination of electromagnetic, strength, and preloading constraints imposed on the system designer. Analysis for design of such structures focuses on the accurate characterization of fluid-structure interaction under dynamic asymmetric loading.


2020 ◽  
Vol 10 (17) ◽  
pp. 5903 ◽  
Author(s):  
Valentina Consolo ◽  
Antonino Musolino ◽  
Rocco Rizzo ◽  
Luca Sani

Multiphysics problems represent an open issue in numerical modeling. Electromagnetic launchers represent typical examples that require a strongly coupled magnetoquasistatic and mechanical approach. This is mainly due to the high velocities which make comparable the electrical and the mechanical response times. The analysis of interacting devices (e.g., a rail launcher and its feeding generator) adds further complexity, since in this context the substitution of one device with an electric circuit does not guarantee the accuracy of the analysis. A simultaneous full 3D electromechanical analysis of the interacting devices is often required. In this paper a numerical 3D analysis of a full launch system, composed by an air-core compulsator which feeds an electromagnetic rail launcher, is presented. The analysis has been performed by using a dedicated, in-house developed research code, named “EN4EM” (Equivalent Network for Electromagnetic Modeling). This code is able to take into account all the relevant electromechanical quantities and phenomena (i.e., eddy currents, velocity skin effect, sliding contacts) in both the devices. A weakly coupled analysis, based on the use of a zero-dimensional model of the launcher (i.e., a single loop electrical equivalent circuit), has been also performed. Its results, compared with those by the simultaneous 3D analysis of interacting devices, show an over-estimate of about 10–15% of the muzzle speed of the armature.


1986 ◽  
Vol 22 (6) ◽  
pp. 1536-1541 ◽  
Author(s):  
E. Igenbergs ◽  
S. Aigner ◽  
A. Hudepohl ◽  
M. Rott ◽  
U. Weishaupt ◽  
...  

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