The Aeroelastic Divergence of Unguided Missiles by Dynamics Analysis,

Abstract

A method of determining aeroelastic divergence conditions by dynamic analysis for unguided missiles is presented in this report. A sample problem has been calculated and aeroelastic divergence parameters investigated. The computer program is included along with user instructions. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 02, 1971
Accession Number
AD0732477

Entities

People

  • Gerald W. Rister
  • Joe C. Walters

Organizations

  • United States Army Aviation and Missile Command

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Computer Programs
  • Computers
  • Dynamics
  • Instructions
  • Transient Response Analysis

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Atmospheric Science/Meteorology
  • Ballistic Missile Meteorology