Acoustic Pulse Scattering from Impedance Covered Cylinders.

Abstract

An expression for the acoustic scattered pressure from an impedance covered cylinder due to an incident plane pulse is obtained analytically. The application of Fourier transform on time and subsequent Sommerfield-Watson transformation results in separate expressions for geometrically reflected pressure and for creeping (or circumferential) waves. Using Cauchy contour integration theorem and saddle-point methods, the inverse Fourier transform is evaluated. The impulse response and convolution theorem have been utilized to obtain an expression for the scattered pressure for incident harmonic pulse train and FM pulses. The first arrival of acoustic wave at an observer point in the far field is shown to be due to the geometrically reflected pressure. After the first arrival, creeping waves are shown to circumnavigate the cylinder surface for an indefinite number of times and radiate off tangentially at any angle. These waves create the multiple echoes that return in the scattering of a single pulse. The circumferential waves are shown to decay exponentially as they encircle the cylinder surface. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1983
Accession Number
ADA131653

Entities

People

  • Abbas Khavaran

Organizations

  • Pennsylvania State University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Acoustic Propagation
  • Acoustic Waves
  • Acoustics
  • Complex Variables
  • Diffraction
  • Equations
  • Far Field
  • Frequency
  • Geometry
  • Integral Equations
  • Integrals
  • Pennsylvania
  • Plane Waves
  • Resonant Frequency
  • Scattering
  • Step Functions
  • Universities

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Radar Systems Engineering.