Elsevier

Annals of Physics

Volume 6, Issue 3, March 1959, Pages 277-299
Annals of Physics

On the theory of scalar diffraction and its application to the prolate spheroid

https://doi.org/10.1016/0003-4916(59)90083-1Get rights and content

Abstract

Scalar scattering of a plane wave by a perfectly reflecting body whose surface is a level surface in a coordinate system in which the scalar wave equation is separable is considered. A general method for the computation of the surface distribution is described. This method reduces the problem of finding the surface distribution to that of evaluating a certain contour integral. The distribution induced on a prolate spheroid by an axially-symmetric plane wave is specifically computed. The evaluation by residues of the contour integral, given by the general theory, leads to the expected “creeping wave” interpretation of the residue series in which the attenuation of the “creeping waves” depends, in first approximation, on the local radius of curvature. The asymptotic theory used is applicable for large values of cω, where 2c is the interfocal distance of the spheroid and ω is the wave number. The surface distribution is computed over the entire shadow region including the tip.

References (15)

  • J.B. Keller

    Trans. I.R.E.

    (1956)
  • A.R. Sims

    J. Math. and Mech.

    (1957)
  • R.S. Phillips

    New York University Research Report EM-42

    (1952)
  • R.K. Ritt

    University of Michigan Report No. 2591-4-T

    (1958)
  • R.E. Langer

    Trans. Am. Math. Soc.

    (1932)
  • R.E. Langer

    Trans. Am. Math. Soc.

    (1935)
  • V.A. Fock et al.

    J. Phys. (USSR)

    (1946)
There are more references available in the full text version of this article.

Cited by (11)

  • Diffraction by an Elliptic Cylinder

    2023, Springer Series in Optical Sciences
  • High-frequency scattering from rigid prolate spheroids

    1988, Journal of the Acoustical Society of America
View all citing articles on Scopus

The research reported in this paper has been sponsored by the Air Force Cambridge Research Center, Air Research and Development Command, Contract AF-19(604)-1949.

View full text