Dynamics of the Design of a Flight Vehicle

Abstract

The book is devoted to the problem of determining the necessary carrying capacity and rigidity of design of a flight vehicle. Discussed in it are theoretical bases and practical methods of the calculation of internal force factors from external forces acting on the vehicle in the process of operation, and methods of development of calculation cases of loading are given. In this case the main attention is given to problems of the dynamics of design, in particular the selection of design configurations, the formulation of equations of dynamic equilibrium and determination of the dynamic reaction of design on the effect of external perturbations. Consideration is given to those limitations which are imposed by conditions of strength of the design on values of certain parameters of the propulsion system, automatic control system, complex of ground equipment, and also on conditions of operation of flight vehicles of different types.

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Document Details

Document Type
Technical Report
Publication Date
Aug 05, 1970
Accession Number
AD0712822

Entities

People

  • V. F. Gladkii

Organizations

  • Air Force Systems Command

Tags

Communities of Interest

  • Ground and Sea Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeroelasticity
  • Aircrafts
  • Atmospheric Motion
  • Boundary Layer
  • Computational Science
  • Control Systems
  • Differential Equations
  • Dynamic Loads
  • Elastic Properties
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Mechanical Properties
  • Mechanical Working
  • Mechanics
  • Modulus Of Elasticity
  • Propulsion Systems

Fields of Study

  • Engineering

Readers

  • Control Systems Engineering.
  • Software Engineering