Vadim G. Structurally-technological method of increasing the fatigue life of detachable bolted joints of airframe structural members

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0410U006397

Thesis Registration Form

0410U006397.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

16-12-2010

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

Object - designing and manufacturing of airframe structural members with consideration of fatigue; the purpose - increasing the fatigue life and service life of detachable bolted joints of airframe structural members; new development - structurally-technological method of increasing the fatigue life and service life of detachable bolted joints of airframe structural members by improvement of technique of calculation of airframe structural members local mode of deformation characteristics in the area of detachable bolted joints is newly developed, further development of the technique of the fatigue life and service life of detachable bolted joints of airframe structural members prediction has been provided; the field is Airplane and Rocket production.

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Files

aref.doc

aref.doc

dis.doc

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