Study on Panels of Aircraft Structures under Repeated Static Loads,

Abstract

The brief conclusion drawn in the report concerning the effect of structural and technological factors on the durability of various structures are approximate and describe a structure only from the standpoint of applying variable loads of different magnitudes. For this reason further comprehensive studies are required. Nevertheless, the general regularities revealed in this article can be used in designing aircraft structures which are calculated for a long service life under variable loads.

Document Details

Document Type
Technical Report
Publication Date
Oct 09, 1973
Accession Number
AD0768457

Entities

People

  • B. I. Sakharov
  • E. P. Obolenskii

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Loads (Forces)
  • Mechanical Structure
  • Resilience
  • Static Loads

Fields of Study

  • Engineering

Readers

  • Control Systems Engineering.
  • Educational Psychology
  • Facility/Structural Engineering.