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The issue contains the following articles:

Comparison of the flight loads spectra of two business jets; Wireless energy supply to aircraft structural helath monitoring nodes using ultrasonic lamb waves; Synchrotron radiation application for lattice strain measurement; Comparison of selected rivet and riveting instructions; The analysis of the influence of riveting parameters specified in selected riveting instructions on residual stresses; Fatigue properties of polyurethane foams, with special emphasis on authentic foams, used for helicopter pilot seat cusion inserts; The concept of a full scale fatigue test of a SU-22 fighter bomber; Selected aspects related to preparation of a fatigue test plan of a metalic airframe; Selected aspects related to preparation of fatigue tests of a metallic airframe; Selected aspects related to the applied loads control during fatigue tests of a metallic airframe; Stress analysis of the PZL M 28'S airframe subjected to repairs during fatigue tests; An approach to structural health monitoring of composite structures based on embedded PZT transducers; Simulationg crack propagation of a selected structural component of the PZL-130 Orlik TC-II aircraft

Other issues of the magazine are available at: http://www.degruyter.com/view/j/fas

Nazwa publikacji: Fatigue of Aircraft Structures ISSUE 2013
Autor: editor Antoni Niepokólczycki
ISBN/ISSN: 2300-7591
Oprawa: miękka
Data publikacji: 2015-08-07
Wydawnictwo: Wydawnictwa Naukowe Instytutu Lotnictwa
Liczba stron: 127
Wydanie: angielski