[[1] Reymer, P., Leski, A. and Dragan, K., (2012). Recent Progress in Full Scale Fatigue Test of PZL-130 “Orlik” TC-II Structure, Fatigue of Aircraft Structures, Vol. 1, pp. 76-81.]Search in Google Scholar
[[2] Reymer, P., Leski, A., Zielinski, W. and Jankowski, K., (2015). Full Scale Fatigue Test concept of a Su-22 fighter bomber, Fatigue of Aircraft Structures, Warsaw, 2015, vol. 6, pp. 79-87.]Search in Google Scholar
[[3] Leski A., Reymer P., Kurdelski M. (2011). Development of Load Spectrum for Full Scale Fatigue Test of a Trainer Aircraft. In: Komorowski J. (eds) ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives. Springer, Dordrecht.]Search in Google Scholar
[[4] Kottkamp, E., Wilhelm, H. and Kohl, D., (1976). Strain gauge measurements on aircraft, NATO Advisory Group for Aerospace Research and Development, AGARDograph No. 160, Vol. 7.]Search in Google Scholar
[[5] Jenkins, J. M. and DeAngelis, V. M., (1997). A summary of numerous strain-gage load calibrations on aircraft wings and tails in a technology format, Nasa Technical memorandum 4804, Edwards, California.]Search in Google Scholar
[[6] Skopionski, T.H., Aiken Jr., W. S. and Huston, W. B., (1954). Calibration of strain-gage installations in aircraft structures for the measurement of flight loads, NACA Technical Report 1178.]Search in Google Scholar
[[7] Dowodztwo Wojsk Lotniczych (1989). Smiglowiec Mi-24W. Opis techniczny. Ksiazka 2 – Platowiec i zespol napedowy, Poznan.]Search in Google Scholar
[[8] Lesniczak, A. et al., (2019). Warunki techniczne na wykonanie pelnoskalowej proby dowodowej struktury smiglowca Mi-24, ITWL, WT-81-/31/2019.]Search in Google Scholar
, 