[Nesterenko, G. I. (2000). In: Proceedings of the 22nd International Council of the Aeronautical Sciences. Comparison of Damage Tolerance of Integrally Stiffened and Riveted Structures, 27 August - 1 September 2000, Harrogate, United Kingdom: ICAS.]Search in Google Scholar
[Krueger, R. (2002). The Virtual Crack Closure Technique: History, Approach and Applications. Hampton: NASA Langley Research Center. (NASA/CR-2002-211628)]Search in Google Scholar
[NASGRO Reference Manual, Version 4.2. San Antonio: NASA Johnson Space Center, Southwest Research Institute.]Search in Google Scholar
[Lanciotti, A., Lazzeri, L., & Polese, C. (2005). Description of the Test Programme, DaToN - WD - WP 3.1 - 1.0 / DIA. Pisa: University of Pisa.]Search in Google Scholar
[Jonge, J. B. de, Hol, P. A., & van Gelder, P. A. (1994). Reanalysis of European Flight Loads Data., DOT/FAA/CT-94/21, Atlantic City: FAA, Technical Center.]Search in Google Scholar
[Rustenberg, J., Skinn, D., & Tipps, D. O. (1998). Statistical Loads Data for Boeing 737-400 Aircraft in Commercial Operations. Washington: FAA, Office of Aviation Research. (DOT/FAA/AR-98/28)]Search in Google Scholar
[Skinn, D., Tipps, D. O., & Rustenberg, J. (1998). Statistical Loads Data for MD-82/83 Aircraft in Commercial Operations. Washington: FAA, Office of Aviation Research. (DOT/FAA/AR-98/65)]Search in Google Scholar
[Tipps, D. O., Rustenberg, J., & Skinn, D. (2000). Statistical Loads Data for Boeing 767-200ER Aircraft in Commercial Operations. Washington: FAA, Office of Aviation Research. (DOT/FAA/AR-00/18)]Search in Google Scholar
[Crabill, N. L. (1989). The NASA Digital VGH Program - Exploration of Methods and Final Results, Volume III - B727 Data 1978-1980: 1765 Hours. Hampton: NASA CR-181909.]Search in Google Scholar
[Crabill, N. L. (1989). The NASA Digital VGH Program - Exploration of Methods and Final Results, Volume IV - B747 Data 1978-1980: 1689 Hours. Hampton: NASA CR-181909.]Search in Google Scholar
[de Jonge, J. B., Schütz, D., Lowak, H., & Schijve, J. (1973). A Standardized Load Sequence for Flight Simulation Tests on Transport Aircraft Wing Structures, Amsterdam, Netherlands: National Aerospace Laboratory. (NLR TR 73029U)]Search in Google Scholar
[Lanciotti, A., & Lazzeri, L. (1992). Effects of Spectrum Variations on Fatigue Crack Growth. International Journal of Fatigue, 14(5), 319-324.10.1016/0142-1123(92)90483-S]Search in Google Scholar
[Akdenitz, A. (2001). The Impact of Mandated Aging Airplane Programs on Jet Transport Airplane Scheduled Structural Inspection Programs. Aircraft Engineering and Aerospace Technology, 73(1), 4-15.10.1108/00022660110366827]Search in Google Scholar
[Abelkis, P. R. (1980). Effect of transport aircraft wing loads spectrum variation on crack growth. In D.F. Bryan & J.M. Potter (Eds.). Effect of Load Spectrum Variables on Fatigue Crack Initiation and Propagation, ASTM STP 714, (pp.143-169). Philadelphia: American Society for Testing and Materials.]Search in Google Scholar