Accession Number : AD0768457

Title :   Study on Panels of Aircraft Structures under Repeated Static Loads,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Obolenskii,E. P. ; Sakharov,B. I.

Report Date : 09 OCT 1973

Pagination or Media Count : 31

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.

Descriptors :   (*AIRFRAMES, FATIGUE(MECHANICS)), STRESSES, LOADS(FORCES), BENDING, FAILURE(MECHANICS), PROBABILITY, REGRESSION ANALYSIS, USSR

Subject Categories : Aircraft
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE