Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Rustam Yarullin"'
Publikováno v:
Fatigue & Fracture of Engineering Materials & Structures. 45:2854-2872
Publikováno v:
Frattura ed Integrità Strutturale, Vol 14, Iss 53, Pp 210-222 (2020)
Frattura ed Integrità Strutturale; Vol. 14 No. 53 (2020): July 2020; 210-222
Frattura ed Integrità Strutturale; V. 14 N. 53 (2020): July 2020; 210-222
Frattura ed Integrità Strutturale; Vol. 14 No. 53 (2020): July 2020; 210-222
Frattura ed Integrità Strutturale; V. 14 N. 53 (2020): July 2020; 210-222
In this paper, a procedure to calculate stress intensity factors for imitation models of titanium alloys is proposed. Fatigue cracks are detected in a disk and blade dovetail type attachment in service. Based on the attachment dimensions and taking i
Autor:
Mikhail Yakovlev, Rustam Yarullin
Publikováno v:
Frattura ed Integrità Strutturale; Vol. 16 No. 60 (2022): April 2022; 451-463
Frattura ed Integrità Strutturale; V. 16 N. 60 (2022): April 2022; 451-463
Frattura ed Integrità Strutturale; V. 16 N. 60 (2022): April 2022; 451-463
In this paper the fatigue crack growth tests were carried out on surface-crack tension (SCT) specimens, made of 7050 and Ti6Al4V alloys, with initial semi-elliptical surface cracks. Pure Mode I conditions were realized on SCT specimens with crack pla
Publikováno v:
MATEC Web of Conferences, Vol 300, p 11009 (2019)
The experimental study of heat flux evolution at the fatigue crack tip during biaxial loading was carry out in this work. The plane samples of stainless steel AISI 304 with thick of 3 mm were weakened by notch to initiate fatigue crack at the centre
Three-dimensional numerical analyses, using the finite element method (FEM), have been adopted to simulate fatigue crack propagation in a hollow cylindrical specimen, under pure axial or combined axial-torsion loading conditions. Specimens, made of A
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::884f6e5a23379646d430464a8a469d8a
http://hdl.handle.net/11588/751268
http://hdl.handle.net/11588/751268
Publikováno v:
MATEC Web of Conferences, Vol 300, p 11001 (2019)
This study is concerned with analysis of fatigue crack growth and life-time prediction for aviation GTE compressor disk under operation conditions. For consideration were different combinations of rotational speed, temperature, surface flaw form and