The pattern of magnetic-source on the surface of an infinite length conducting circular cylinder coated with a dielectric

Author(s):  
M. Zhiji ◽  
W. Jianxiang
1986 ◽  
Vol 53 (4) ◽  
pp. 929-934 ◽  
Author(s):  
K. G. Sorenson ◽  
J. B. Cheatham

An axially loaded weightless circular rod buckles helically when constrained within a circular cylinder. The effects of pinned and fixed-end conditions are investigated. Both end conditions locate the rod end on the cylinder axis, and are found to perturb the helix in an exponentially decaying manner for a distance of less than one helix pitch length. Far from the end, the rod behaves as an undisturbed constant-pitch helix. The distance from the rod end to the point of initial contact with the cylinder wall is calculated. Closed-form analytical solutions are obtained for the deflected shapes and internal reactions of the end sections. The solution procedure applies to rods of either finite or infinite length.


1956 ◽  
Vol 34 (2) ◽  
pp. 190-202 ◽  
Author(s):  
James R. Wait ◽  
K. Okashimo

Theoretical radiation patterns are presented for radial electric dipoles located on an isolated circular cylinder, and a cylindrically tipped half-plane. These cylindrical structures are considered to be of infinite length and of perfect conductivity. The computed patterns for the isolated cylinder compare well with the experimental results reported by Bain.


1955 ◽  
Vol 33 (5) ◽  
pp. 189-195 ◽  
Author(s):  
James R. Wait

A solution is given for the problem of a plane wave incident obliquely on a circular cylinder of infinite length. The electric properties of the cylinder are taken to be homogeneous and isotropic but otherwise arbitrary. It is shown that in the general case the scattered field contains a significant cross-polarized component which vanishes at normal incidence. While the solution is derived for the magnetic vector of the incident wave transverse to the axis of the cylinder, the corresponding result for the other polarization can be obtained from symmetry.


1980 ◽  
Vol 24 (01) ◽  
pp. 1-7
Author(s):  
Monir F. George

Exact analytic expressions are presented for the induced velocity components at any field point due to a single vortex ellipse and due to a vortex elliptic cylinder of uniform strength with a finite and a semi-infinite length. The elliptic cylinder is assumed to deviate very little from the reference circular cylinder. Comparison is made between the derived expressions and those due to a semi-infinite vortex circular cylinder, and sample calculations are presented. This investigation has a direct application to the case of nonaxisymmetric annular aerofoils of elliptic cross sections.


The problem of determining the critical conditions in a non-circular cylinder of infinite length is examined, in which the reaction is of zero order and where the Frank-Kamenetskii approximation to the reaction rate has been made. The generators are assumed parallel and the boundary of a cross section is given by r = 1 + ε cos θ ( ε ≪ 1), where ( r , θ ) are plane polar coordinates. The surface conditions assumed are (i) uniform temperature and (ii) newtonian cooling. By suitable expansions of the interior temperature and the Frank-Kamenetskii parameter δ , it is shown that the critical value of δ for (ii) is δ crit ( ε, B ) = 8 σ c /(1 + σ c ) 2 exp[ – (4 σ c )/ B (1 + σ c )] x [1 - ε 2 { σ 2 c /1 + σ c ) + (1/ B ) σ c (1 + 3 σ c )/(1 + σ c ) 2 } + O ( ε 4 )], Where σ c = -2/ B + (1 + 4/ B 2 ) ½ and where B is a Biot number propor­tional to the surface-heat transfer coefficient. For (i), the simple result δ crit ( ε , ∞) = 2 - ε 2 + O ( ε 4 ), is obtained.


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