Zobrazeno 1 - 10
of 29
pro vyhledávání: '"Wronicz, Wojciech"'
Autor:
Leski Andrzej, Wronicz Wojciech, Kowalczyk Piotr, Szmidt Michał, Klewicki Robert, Włodarczyk Karol, Uliński Grzegorz
Publikováno v:
Fatigue of Aircraft Structures, Vol 2020, Iss 12, Pp 78-91 (2020)
The Modular Test Stand was developed and manufactured to decrease the cost of fatigue testing and reduce the time of its completion as well as to enable testing specimens under more complex load conditions. The stand consists of three connected secti
Externí odkaz:
https://doaj.org/article/a4657c2bea894e6e9b91a97503879529
Autor:
Wronicz, Wojciech, Malicki, Maciej
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2018, Vol. 91, Issue 2, pp. 235-240.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-01-2018-0040
Autor:
Wronicz Wojciech
Publikováno v:
Fatigue of Aircraft Structures, Vol 2018, Iss 10, Pp 63-72 (2018)
Rivets are critical areas in metal airframes from the fatigue point of view. Fatigue behaviour of riveted joints depends strongly on the residual stress system around the rivet holes. The both most convenient and most common method of determining the
Externí odkaz:
https://doaj.org/article/74a7caac2b4f4ae69eac5c3e1a9096ea
Publikováno v:
Fatigue of Aircraft Structures, Vol 2017, Iss 9, Pp 157-170 (2017)
Fatigue behaviour is one of the most important properties of modern airplanes and rivets influence it strongly. According to the literature, the NACA riveting offers a multiple increase in the fatigue life of joints.
Externí odkaz:
https://doaj.org/article/aada6c8df55348e59304e661d7872c6e
Autor:
Wronicz Wojciech
Publikováno v:
Fatigue of Aircraft Structures, Vol 2016, Iss 8, Pp 116-126 (2016)
One crucial characteristic of the aircraft structure are fatigue properties and rivets are usually critical areas in metal airframes due to fatigue cracks nucleation. According to literature, the NACA riveting method offers a huge increase in fatigue
Externí odkaz:
https://doaj.org/article/be49cedeee634de695f2d2a3b142b9f8
Publikováno v:
Fatigue of Aircraft Structures, Vol 2016, Iss 8, Pp 73-79 (2016)
Measuring the in-depth stress state is of vital importance for materials scientists. Strain gauges methods are capable of yielding information only about the surface stress state. Diffraction methods using synchrotron or neutron radiation, which allo
Externí odkaz:
https://doaj.org/article/d216e66b8bb048dc8dc7d81c7eb18a8a
Autor:
Gadalińska Elżbieta, Wronicz Wojciech
Publikováno v:
Fatigue of Aircraft Structures, Vol 2016, Iss 8, Pp 65-72 (2016)
Electropolishing is the sole reliable method of removing the outer layer of the specimen without changing its stress state. This feature of the electropolishing procedure allows researchers to investigate the in-depth stress distribution. Developing
Externí odkaz:
https://doaj.org/article/62e791b94a3747539dd7f7fa081b8a90
Autor:
Kaniowski Jerzy, Wronicz Wojciech
Publikováno v:
Fatigue of Aircraft Structures, Vol 2013, Iss 5, Pp 66-78 (2014)
The paper presents experimental and numerical study of the local phenomena during the riveting process.
Externí odkaz:
https://doaj.org/article/98c0e40900ed4f9ca4fdb58c04c55efd
Autor:
Wronicz Wojciech, Kaniowski Jerzy
Publikováno v:
Fatigue of Aircraft Structures, Vol 2014, Iss 6, Pp 63-71 (2014)
The riveting parameters strongly affect residual stresses induced during riveting, which in turn have an impact on the fatigue life of riveted joints. Since rivets are established as critical from the fatigue point of view, the fatigue life of rivete
Externí odkaz:
https://doaj.org/article/b761a8a2d105493fa9f813968f0cf368
Publikováno v:
Fatigue of Aircraft Structures, Vol 2015, Iss 7, Pp 66-68 (2015)
The application of a new type of alloy requires the evaluation of its properties, which is typically achieved with destructive methods. For this purpose, among others, static and fatigue mechanical tests are performed. Tests are performed on standard
Externí odkaz:
https://doaj.org/article/0431d9973a2b40a3ba4dc05051bd6b3d