Vesel's'kyj S. Designing and experimental finishing of wing reinforced plane panels in caisson system unter compound loading.

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0400U001601

Thesis Registration Form

0400U001601.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

23-05-2000

Specialized Academic Board

Д 64.062.03ё

Essay

The thesis contains the new theoretical and practical results on designing reinforced with plane wing stringer set panels under compound loding compression and shear. There were developend the technologies, algonithms and program of panel designing, orinttd to be used computer based designing systems. The new concept of testing the panejs in the wing caisson system has been realised on original stands for full-scale and model panels investigation. The test of series of experimental panels has been camed out which confirmed the theoretical results. The main results have been applied on ASTC ''Antonov" and are being used on other enterprises and organisations.

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