Zobrazeno 1 - 10
of 23
pro vyhledávání: '"B. A. Nesterenko"'
Autor:
B. G. Nesterenko, G. I. Nesterenko
Publikováno v:
Научный вестник МГТУ ГА, Vol 0, Iss 199, Pp 11-22 (2017)
Analysis of US and Russia Regulations on fatigue and damage tolerance of transport aircraft structures is given. The methods to provide the safe operation of aging aircraft in Russia are presented for cases of multiple site damages, corrosion and mat
Externí odkaz:
https://doaj.org/article/4f2b7ae5e7414a629e543aec64470579
Development of top-level requirements for regional aircraft based on the needs of the Russian market
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 1024:012070
The share of regional flight traffic is estimated as 10% of all air transport network in Russian Federation. According to the federal plans on infrastructure improvement, the regional aviation in Russia should provide public transport accessibility o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0d9e408a3b04d05dc1b3399756bdeb17
https://doi.org/10.1088/1757-899x/1024/1/012070
https://doi.org/10.1088/1757-899x/1024/1/012070
Autor:
B. G. Nesterenko, G. I. Nesterenko
Publikováno v:
Journal of Machinery Manufacture and Reliability. 42:114-123
Permissible stresses for wing and fuselage structures are given for passenger (transport) aircraft according to fatigue, fail-safe, and damage tolerance criteria. Permissible fatigue stresses are determined for securing the lifetime of modern aircraf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::91469a0a4866023857060a84456f4b33
https://doi.org/10.3103/s1052618813020118
https://doi.org/10.3103/s1052618813020118
Autor:
G. I. Nesterenko, B. G. Nesterenko
Publikováno v:
Journal of Machinery Manufacture and Reliability. 42:62-75
Fatigue and survivability requirements for transport aircraft structures formulated in the US Federal Aviation Regulations FAR 25.571, Advisory Circular AC 20-107B and in the Russian Aviation Regulations AR 25.571 are analyzed. Information on the lif
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::852157dacc9d86950f39848beeec496a
https://doi.org/10.3103/s1052618813010093
https://doi.org/10.3103/s1052618813010093
Autor:
B. G. Nesterenko
Publikováno v:
Journal of Machinery Manufacture and Reliability. 40:176-189
The fulfillment of the standard requirements for fatigue and damage tolerance of aircraft structures is the basis for ensuring their safe operation. The paper analyzes the rules formulated in the U.S. FAA Standards and Recommendation Circulars, Sovie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47e82e6fb6dbdcbbe9ea8691e350d4de
https://doi.org/10.3103/s1052618811020117
https://doi.org/10.3103/s1052618811020117
Autor:
B. G. Nesterenko
Publikováno v:
Journal of Machinery Manufacture and Reliability. 39:605-611
The development of methods and principles of foreign and domestic regulatory requirements that ensure the safe operation of civilian aircraft is considered.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::731ffcaa08dd12c975a6acf5af92d1c0
https://doi.org/10.3103/s1052618810060154
https://doi.org/10.3103/s1052618810060154
Publikováno v:
Journal of Machinery Manufacture and Reliability. 37:408-411
Experimental studies of the fatigue and durability of panels forming a longitudinal lap joint of the fuselage skin are considered. Correction factors for calculating strain intensities, panel durability until crack formation, the duration of the proc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::730ffa5df431cd0dc65d34f4404d49a7
https://doi.org/10.3103/s1052618808040158
https://doi.org/10.3103/s1052618808040158
Autor:
B. G. Nesterenko
Publikováno v:
Journal of Machinery Manufacture and Reliability. 36:547-553
A method for calculating the residual strength of a stiffened structure (panel) taking into account the stable growth of a crack is presented. The use of the R curve of material is based on experimental data. Calculated results are compared with expe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6c70c2c38ab7768c572a50c2897f6cb9
https://doi.org/10.3103/s1052618807060076
https://doi.org/10.3103/s1052618807060076
Autor:
B. G. Nesterenko
Publikováno v:
Journal of Machinery Manufacture and Reliability. 36:450-453
A definition of kinetic diagrams of fatigue crack propagation in aluminum alloys for various loading cycle asymmetries is considered. Calculations and experimental measurements of crack propagation time for upper and lower wing skins are presented; t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3167e010be7cb6f3064b6bfa2a90beb9
https://doi.org/10.3103/s1052618807050111
https://doi.org/10.3103/s1052618807050111
Publikováno v:
Strength of Materials. 38:398-403
We present the results of experimental investigations of the mechanical characteristics, fatigue characteristics, cyclic crack growth resistance and residual strength of aluminum alloy materials for a wing and fuselage skin of airplanes having a serv
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a1b307d705436c4db08f1314bb578a17
https://doi.org/10.1007/s11223-006-0056-z
https://doi.org/10.1007/s11223-006-0056-z