Galunenko O. Cardo aeroplane designing taking into account the possibility of powered landing realization

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0400U002455

Thesis Registration Form

0400U002455.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

22-09-2000

Specialized Academic Board

Д 64.062.03

Essay

The thesis contains the results of theoretical and practical investigations on developing the new algorithms of providing the exact landing parameters of transport aeroplanes in the STL regime. The methods and the algorithms were approved on the testing flight stand of ASTK "Antonov" and applied in the first stage of the flight test of An-70 in the STL regime.

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