The External Loads and Strength of Flying Apparatuses

Abstract

This book is dedicated to external loads having effect on a flight vehicle (aircraft and helicopter), and the durability of its construction. Basic attention in the book is allotted to actual problems of strength of contemporary flight vehicles: dynamic load, periods of service and strength of construction, strength during high speeds of flight, taking into account aerodynamic heating and others. Along with an account of theoretical questions in the book there are described experimental methods of investigating strength of construction. The book is designed for engineers connected with designing, tests, and exploitation of flight vehicles. At the same time, it can be used as a training aid for aviation students of higher educational institutions.

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Document Details

Document Type
Technical Report
Publication Date
Jul 20, 1965
Accession Number
AD0622400

Entities

People

  • A. I. Gudkov
  • L. G. Ryakov
  • P. S. Leshakov

Organizations

  • Air Force Systems Command

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Birds
  • Boundary Layer
  • Computational Science
  • Convection
  • Equations Of Motion
  • Fluid Dynamics
  • Heat Transfer
  • Jet Aircraft
  • Measurement
  • Mechanical Properties
  • Mechanics
  • Spars
  • Test And Evaluation

Readers

  • Aerodynamics/Aeronautics.
  • Structural Health Monitoring of Composite Structures.
  • Systems Analysis and Design