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REFERENCES [1] Fatemi A., Yang L.: Cumulative fatigue damage and life prediction theories: a survey of the state of the art for homogeneous materials . Int. J. of Fatigue, vol. 20, nº 1, pp. 9-34, 1998. [2] Schijve, J.: Fatigue of structures and materials in the 20th century and the state of the art . Materials Science, vol. 39, nº 3, pp. 307-333, 2003. [3] Debski M., Debski D.: Selected problems of fatigue strength of aircraft structures. Scientific Library of the Institute of Aviation 36, ISBN 978-83-63539-06-1, Warsaw 2014. [4] Szala J.: Hypotheses of

REFERENCES [1] Brzęczek J, Gruszecki H, Pieróg L, Pietruszka J. Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe. Fatigue of Aircraft Structures. Issue 2014. Institute of Aviation Scientific Publications, Warsaw, Poland. [2] Brzęczek J, Gruszecki H, Pieróg L, Pietruszka J. Selected Aspects Related to Preparation of Fatigue Tests of a Metallic Airframe. Fatigue of Aircraft Structures. Issue 2014. Institute of Aviation Scientific Publications, Warsaw, Poland. [3] Brzęczek J, Chodur J, Pietruszka J. Selected Aspects Related

References [1] Barter S.A., Molent L., Wanhill R.J.H.(2009). Marker loads for quantitative fractography of fatigue cracks in aerospace alloys. Proceedings of the 25th ICAF Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, The Netherlands, May 2009, p. 15-54 [2] Wanhill R.J.H., Barter S.A. (1994). NLR Technical Publication TP 94177 U, National Aerospace Laboratory NLR , Amsterdam, 1994. [3] Podskarbi S. (2010). Dokumentacja techniczna z zabudowy czujników tensometrycznych na płatowcu PZL-130 Orlik TC-II nr boczny 037 . Warszawa: ITWL

References AWS., 1987. Welding Handbook, Volume 1. 8th ed. pp.231-233. Bannantine, J.A., Comer, J.J. and Handrock, J.L., 1990. Fundamentals of Metal Fatigue Analysis. Prentice-Hall, Inc. Gurney, T.R., 1979. Fatigue of Welded Structure. 2nd ed. Cambridge University Press. Kim, H., 1992. A study on the fatigue crack opening behavior of the material with welding residual stress field. PhD. Korea University. Kim, W.S., 1997. Residual Stress & Fatigue strength in Welded Ship Structure. Journal of KWS, June , 15(3). Kim, Y.S., 1989. The Welding Residual Stress and

References United States Air Force. (1978, January). Individual Aircraft Tracking Methods for Fighter Aircraft Utilizing Counting Accelerometer Data. Ohio: Air Force Flight Dynamics Lab. Wright-Patterson Air Force Base. (AFFDL-TM-78-1-FBE) FAA. (1973). Fatigue Evaluation of Wing and Associated Structure on Small Airplanes. (AFS-120-73-2) Veldman Ray J. & Peckham C. (1982, October). Loads and Dynamics Branch Structures Division. In Handbook of Military Aircraft Design Normal Load Factor Exceedance Data. Ohio: Aeronautical Systems Division Wright

, Atlanta, Georgia, (Bigelow, C., editor), National Technical Information Service, Springfield, Virginia 22161, USA, (1996) pp. 129-146 [5] Bray, G.H., Bucci, R.J., Colvin E.L., and Kulak, M., ASTM STP 1298, (Van Der Sluys, W.A., Piascik, R.S., and Zawierucha, R., editors), American Society for Testing and Materials, (1997) pp. 89-103 [6] Zamber, J.E. and Hillberry, B.M. (1999). Probabilistic approach to predicting fatigue lives of corroded 2024-T3. AIAA Journal, 37, 1311-1317 [7] Chubb, J.P., Morad, T.A., Hockenhull, B.S., Bristow, J.W., The effect of exfoliation

REFERENCES 1. J. Pietruszka “Full-Scale Fatigue Tests of PZL M28 05 SKYTRUCK Aircraft”. Transactions of Institute of Aviation , 1/2009 (196). Warsaw, 2009. 2. J. Brzęczek, J. Chodur, J. Pietruszka “Selected Aspects Related to Metallic Airframe Fatigue Tests Preparation”. Fatigue of Aircraft Structures , Issue 2014, Institute of Aviation. Warsaw, 2015.

REFERENCES 1. J. Pietruszka “Full-Scale Fatigue Tests of PZL M28 05 SKYTRUCK Aircraft”. Transactions of Institute of Aviation , 1/2009 (196). Warsaw, 2009. 2. “Fatigue, Fail-Safe, and Damage Tolerance Evaluation of Metallic Structure for Normal, Utility, Acrobatic, and Commuter Category Airplanes”. AC 23-13A. FAA. September 29, 2005.

REFERENCES 1. J. Pietruszka “Full-Scale Fatigue Tests of PZL M28 05 SKYTRUCK Aircraft”. Transactions of Institute of Aviation , 1/2009 (196). Warszawa, 2009. 2. L. Pieróg “Evaluation of PZL M28 05 Airplane Service Life”. Ref. no.: DRG/O/W/24/11. PZL internal report. Mielec, 2011. 3. “Fatigue, Fail-Safe, and Damage Tolerance Evaluation of Metallic Structure for Normal, Utility, Acrobatic, and Commuter Category Airplanes”. AC 23-13A. FAA. September 29, 2005.

REFERENCES 1. J. Pietruszka “Full-Scale Fatigue Tests of PZL M28 05 SKYTRUCK Aircraft”. Transactions of the Institute of Aviation , 1/2009 (196). Warsaw, 2009. 2. J. Brzęczek, H. Gruszecki, L. Pieróg, J. Pietruszka “Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe”. Fatigue of Aircraft Structures , Issue 2014, Institute of Aviation. Warsaw, 2015. 3. J. Pietruszka „Fatigue Test of Full Scale Braced Wing and Wing Carry-Through Structure of a Commuter Aircraft” in A. Niepokólczycki ed. “Review of Aeronautical Fatigue Research