Transient Response of Two Fluid-Coupled Cylindrical Elastic Shells to an Incident Pressure Pulse.

Abstract

The transient response of a system of two initially concentric circular cylindrical elastic shells coupled by an ideal fluid and impinged by an incident plane pressure pulse is studied. The classical techniques of separation of variable and Laplace transforms are employed for simultaneously solving the wave equations governing the fluid motions and the shell equations of motion. The transformed solutions are arranged in such a manner that their inverse transforms can be accurately calculated by solving a set of Volterra integral equations in the time domain. A sample calculation of shell response was performed and results are compared to the case in which the outer shell is absent. It is found that the primary effects of a thin outer shell could be estimated by simple asymptotic formulae. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1978
Accession Number
ADA060711

Entities

People

  • Hanson Huang

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Counter WMD
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Acoustic Waves
  • Bessel Functions
  • Computational Science
  • Elastic Shells
  • Engineering
  • Equations
  • Equations Of Motion
  • Integral Equations
  • Integrals
  • Military Research
  • Molecular Dynamics
  • Naval Operations
  • Navy
  • New York
  • Plane Waves
  • Wave Equations
  • Waves

Readers

  • Fluid Dynamics.
  • Structural Dynamics.