Stavychenko V. The method for account of thermal stress-strain state at strength calculation of skin panels made of composite materials

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0411U001038

Thesis Registration Form

0411U001038.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

17-12-2010

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

Object is aircraft skin panels made of composite materials; the aims to improve the reliability composite panels strength calculation which account of thermal stress-strain state and to decrease of experimental studies of materials properties, the methods are mechanics of laminated materials, shallow shells theory, the novelty is development of method for account of stress-strain state of technology and (or) operational origin at the composite panels strength calculation; results - improving reliability of panels strength conclusion, reduction in mechanical tests of samples of material at operational temperatures; the field is airplane and rocket production.

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Files

aref.doc

dis.doc

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