Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Tetiana Maslak"'
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 4sup2, Pp 31-38 (2024)
This paper considers substantiated by experiments the selection of corrosion-preventing compounds for aircraft structures protection. The influence of corrosion-preventing compounds on the service life of typical riveted joints used in fuselages of p
Externí odkaz:
https://doaj.org/article/77a3fad39981465aa79f61739d7d301a
Autor:
Tetiana Maslak, Mikhail Karuskevich
Publikováno v:
Fatigue & Fracture of Engineering Materials & Structures. 46:1211-1214
In order for enterprises not to suffer significant losses by repurposing their activities for the manufacture of products attractive at certain points in time, it is necessary to take into account the compatibility of resource mutual support of the b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0715c9d4dd523a9e1c29c360cf676df4
https://zenodo.org/record/7747005
https://zenodo.org/record/7747005
Autor:
Ievgen Gavrylov, Mikhail Karuskevich, Sergey Ignatovich, Sviatoslav Yutskevych, Tetiana Maslak
Publikováno v:
Fatigue & Fracture of Engineering Materials & Structures. 45:938-941
Autor:
Tetiana Maslak, M. V. Karuskevich
Publikováno v:
Fatigue & Fracture of Engineering Materials & Structures. 44:2913-2916
Autor:
S. R. Ignatovich, Oleg Karuskevich, Łukasz Pejkowski, Tetiana Maslak, Pavol Kurdel, M. V. Karuskevich
Publikováno v:
Fatigue & Fracture of Engineering Materials & Structures. 44:595-598
Publikováno v:
Fatigue & Fracture of Engineering Materials & Structures. 42:2315-2324
Autor:
Pavol Kurdel, Oleg Karuskevich, M. V. Karuskevich, Tetiana Maslak, Łukasz Pejkowski, S. R. Ignatovich
The paper deals with the problem of ultra-light and light aircraft structural health monitoring. The phenomenological basis and engineering decisions for methods to monitor accumulated fatigue damage and to register overstress of aircraft principal s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5800933fab331f91938e31125f6b646d
https://doi.org/10.22541/au.160133398.85007020
https://doi.org/10.22541/au.160133398.85007020
Publikováno v:
MATEC Web of Conferences, Vol 304, p 01020 (2019)
The complexity of analytical and experimental estimation of aircraft components fatigue life is determined by the irregular character of the load’s sequence, a number of stress concentrators, multiaxial stress state. Proposed early multiaxial fatig
Publikováno v:
International Journal of Fatigue. 39:116-121
Two approaches to aircraft fatigue monitoring by the computer-aided analysis of surface structures are described: (a) application of fatigue indicators attached to the aircraft unit; (b) the direct observation of the alclad aluminium alloys surface.