Yutskevych S. Aircraft skin material bearing capacity prediction by surface layer deformation relief evolution performances.

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0411U003111

Thesis Registration Form

0411U003111.pdf

Applicant for

Yutskevych Sviatoslav Sergiyovych

Specialization

05.07.02 - Проектування, виробництво та випробування літальних апаратів

Date of defense

14-04-2011

Specialized Academic Board

Д26.062.06

Essay

The method of aircraft D16AT skin bearing capacity determination is based on alclad surface deformation relief parameters use. For deformation relief investigation was used interfere optical profiler. The developed method allows to predict time of 0,5 mm fatigue crack initiation. The interrelation between the deformation relief evolution parameters under fatigue is established. The model of deformation relief on a material surface formation is developed.

Thesis supervisor

Ignatovich Sergiy Romualdovych

Official opponents

Гребеніков Олександр Григорович
Василевський Євген Тимофійович

Files

aref.doc

diz.doc

Титул.doc

додатки--АКТ 1_Антонов.jpg

додатки--АКТ 2_ДП 410.jpg

додатки--АКТ 3_НАУ.jpg

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