METHODS IN STRUCTURAL DYNAMICS FOR THIN SHELL CLUSTERED LAUNCH VEHICLES

Abstract

A general methodology in Structural Dynamics based on the use of generalized coordinates is presented. These general methods are demonstrated by analysis of some of the problems of slender, conventional, launch vehicles. Applications of the general methodology are also given for complex configurations employing thin shell tanks in clustered arrangements. The methods of structural analysis and vibration analysis that are presented are not restricted to any particular geometry and apply to any complex redundantly coupled structure. To further demonstrate the general methods, a vibration analysis of the clustered Saturn I launch vehicle is presented.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1965
Accession Number
AD0463571

Entities

People

  • J. Stuart Keith
  • J. W. Lincoln

Tags

Communities of Interest

  • Energy and Power Technologies
  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Angular Momentum
  • Computational Science
  • Computer Programs
  • Computers
  • Control Surfaces
  • Control Systems
  • Differential Equations
  • Engineering
  • Geometry
  • Launch Vehicles
  • Mechanics
  • Resonant Frequency
  • Structural Analysis
  • Two Dimensional
  • Vibration

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Missile Defense Systems.
  • Systems Analysis and Design