Подробное описание документа

   Научные основы конструктивных и производственных концепций обеспечения ресурса летательных аппаратов : [монография] / Богуслаев В. О., Бычков С. А., Гребеников О. Г. [и др.] ; Нац. аэрокосмический ун-т им. Н. Е. Жуковского (Харьковский авиационный ин-т) ; пер. Чмовж О. М., Кириленко М. В., Шаповалов С. М. - Харьков : ХАИ, 2019. - 265 с. : ил., табл. - Библиогр.: с. 259-265. - Текст кн. на англ. яз. - ISBN 978-966-662-654-0.

Тhе scientific grounds of integrated design of high-performance aircraft are presented, constructive and technological solutions are given to provide а given life of aircraft in areas of functional openings, shear detachable and non-detachable bolted joints, riveted joints, ways to delay the growth of fatigue cracks in thin-walled structures made of aluminum alloys. Structural and technological methods for increasing the fatigue life of bolted joints of titanium elements of aircraft structures with allowance for fretting соnоsiоn are presented, and the features of assigning the airframe life time of transport aircraft are described.
For scientists and engineers of the aviation industry, as well as teachers, students and post-graduates of aviation universities.