Structural Vibrations in Space Vehicles

Abstract

Study was made of forcing functions and their characteristics, methods of estimating a combined response, and proof tests required to qualify structure and equipment. The report is presented in three parts. Part One discusses the various sources of vibratory energy which can result in vehicle vibration including rocket noise, aerodynamic pressure fluctuations, wind shear and gust, meteorites and direct mechanical coupling. Part Two discusses the prediction of vibratory response through both empirical and analytical approaches, and includes a thorough discussion of the single degree of freedom system, resonance-on-resonance, panels, shells, mobility, generalized force, joint acceptance, correlations and other statistical tools. Part Three contains a discussion of fatigue and malfunction, the properties of an ideal test, implications of and methods for obtaining a simplified composite response and an examination of various test equivalences.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1961
Accession Number
AD0273334

Entities

People

  • K. Eldred
  • R. White
  • William Roberts

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Engineered Resilient Systems
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Boundary Layer
  • Combustion
  • Computational Fluid Dynamics
  • Computational Science
  • Convection
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Mechanics
  • Modulus Of Elasticity
  • Pressure Distribution
  • Resonant Frequency
  • Rocket Engines
  • Test And Evaluation
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • Software Engineering
  • Structural Dynamics.

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers