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The Fatigue Life Assessment of PZL-130 Orlik Structures Based on Historical Usage Data

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

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Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe

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.

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Selected Aspects Related to the Applied Loads Control During Fatigue Tests of a Metallic Airframe

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.

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Selected Aspects Related to Preparation of Fatigue Tests of a Metallic Airframe

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

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Stress Analysis of the PZL M28’s Airframe Subjected to Repairs During Fatigue Tests

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.

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Estimation of Fatigue Properties of Composite Structures

References Rodzewicz, M. (2008). Determination and extrapolation of the glider load spectra. Aircraft Engineering and Aerospace Technology , 80(5), pp. 487-496. Kensche, C., W. (2002). Proposal for a certification procedure of extended sailplane lifetime. Technical Soaring , 26(2), pp. 32-43. Rodzewicz, M. (2009). Fatigue evaluation of high-loaded aeronautical composite structures. Aircraft Engineering and Aerospace Technology , 81(5), pp. 452 - 460.

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Bonded Joint Monitoring of The Composite Aerospace Structures with The Use of Nde and Shm Approach

References Baker. A, Rose F., Jones R.:"Advances in the Bonded Composite Repair of Metallic Aircraft Structure" vol.2, Elsevier 2002; Dragan K., Swiderski W., Studying Efficiency of NDE Techniques Applied to Composite Materials in Aerospace Applications , Acta Physica Polonica A. Vol. 117, No. 5, May 2010; Synaszko. P Badanie sklein w kompozytowych konstrukcjach szybowców i samolotów ultralekkich , Praca dyplomowa magisterska na wydziale MEiL PW. 2008

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Diagnostics of Composite Aircraft Structures Using Non-Destructive Tests with Thermographic, Ultrasound and Acoustic Methods

defektoskopii Wydawnictwo Naukowo - Techniczne Warszawa. Steven M. Shepard, James R. Lhota, Yulin Hou, Tasdiq Ahmed and David Wang Thermographic characterization of composite materials and structures. Thermal Wave Imaging, Inc.

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Composite Aerospace Structure Monitoring with use of Integrated Sensors

, pp. 89-130. [6] Dziendzikowski M., Kurnyta A., Dragan K., Klysz S., Leski A. In situ Barely Visible Impact Damage detection and localization for composite structures using surface mounted and embedded PZT transducers: A comparative study. Mechanical Systems and Signal Processing , 2015, doi:10.1016/j.ymssp.2015.09.021.

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Monitoring of Crack Growth in a Structure Under a Composite Patch

. (2002). Advances is the Bonded Composite Repair of Metallic Aircraft Structure , Vol.1, Victoria, Australia. U.S. Department of Transportation Federal Aviation Administration. (2003). Guidelines for the Development of Process Specifications, Instructions, and Controls for the Fabrication of Fiber-Reinforced Polymer Composites . Office of Aviation Research Washington. (DOT/FAA/AR-02/110) Baker, A., Rose, F. & Jones, R. (2002). Advances is the Bonded Composite Repair of Metallic Aircraft Structure , Vol.2, Victoria

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