Gumenniy A. Integrated Design of Durable Stretched Wing Panels of Transport Aircraft

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0409U001196

Thesis Registration Form

0409U001196.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

27-02-2009

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

Objective: to ensure the assigned service life characteristics of structural load-carrying elements of stretched wing panels of transport aircraft; novelty: a new method of integrated design of durable stretched wing panels of transport aircraft based on their parametric modeling has been developed; the technique of determination of load forces acting on fasteners securing milled skin and stringers of stretched wing panels has been improved; a combined method of successive application of hole wall mandrelling and barrier compression in the form of segmented configuration holes has been developed to ensure fatigue characteristics of structural elements of stretched wing panels in the area of fuel flow holes.

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Files

autoref.doc

autoref.doc

disertaciya.doc

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