This paper presents the results of analytical and test study on fracture behaviour of aluminium alloys applied in lower and upper wing surfaces and in fuselage skin. Characteristics of static strength, fatigue, residual strength and crack growth had been studied. Fatigue and crack growth had been analysed at cyclic loads and at standardized quasi-random load spectra. Fatigue life had been analyzed basing on linear hypothesis of damage accumulation. Crack growth was calculated using linear as well as retardation\acceleration models. Comparison of fracture behaviour of different aluminium alloys had been carried out.
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REFERENCE
Jaap Schijve. Fatigue of Structures and Materials. Second Edition with CD-ROM. Springer, 2008, 621 p.
A.Z. Vorob'ev, B.I. Olkin, V.N. Stebenev, T.S. Rodchenko. Fatigue Strength of Structural Elements. Moscow, Mashinostroyeniye, 1990, 199p. (in Russian).
S.I. Kishkina. Fracture Resistance of Al-alloys. Moscow, Metallurgiya, 1981, 279 p. (in Russian).
I.N. Fridlyander.Al-alloys in Flying Vehicles in the Periods of 1970–2000 and 2001–2015. Journal: Tehnologiya Legkih Splavov, N 4, 2002, VILS, p.12–17 (in Russian).
I.N. Fridlyander, V.V. Sadkov, V.S. Sandler, T.P. Fedorenko. Semiproduct Properties of High-Tech Al-Li-Alloy 1441. Journal: Tehnologiya Legkih Splavov, N 4, 2002, VILS, p.24–26 (in Russian).
United States Patent, 4,294,625. Oct. 13, 1981.
Airliner, April–June 1996, Boeing. Boeing Structural Design and Technology Improvements.
V.N. Basov, G.I. Nesterenko, V.Ye. Strizhius. Typified Loading Program for Heavy Transport. Troudy TsAGI, issue 2642, Moscow, 2001, pp.26–34 (in Russian).
J.B. de Jonge, D. Schütz, D. Lowak and J. Schijve. A Standardized Load Sequence for Flight Simulation Test on Trasport Aircraft Wing Structures. LBF Bericht FB-106, NLR 73029U, 1973.
R.F. Fowler and R.T. Watanabe. Development of Jet Transport Airframe Test Spectra. Boeing Commertial Airplanes, Seattle, Wahington, USA, May 1989, 16 p.
J.P. Gallagher, P.C. Miedlar, C.W. Cross, M.L. Papp. Cracks 93 System User's Manual. University of Dayton Research Institute, UDR-TR-93-107.
V.N. Basov, G.I. Nesterenko. Fatigue Strength of Al-Alloys under Irregular Loading. Troudy TsAGI, issue 2669, Moscow, 2005, pp.119–125 (in Russian).
V.N. Basov, B.G. Nesterenko, G.I. Nesterenko. Fracture of High-Strength Al-Alloys. All-Russian Scientifica Journal: Polyet, 2008, “Mashinostroyenie-Polyet”, pp. 87–92. (in Russian).
V.N. Basov, B.G. Nesterenko, G.I. Nesterenko, V.G. Petrusenko. Experimental Study of Airplane Long Operation Effect on Degradation of Mechanic properties, fatigue strength and crack resistance of applied Al-alloys. Troudy TsAGI, issue 2669, Moscow, 2005, pp.126–142 (in Russian).
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Nesterenko, B., Nesterenko, G.I., Basov, V.N. (2009). Fracture Behaviour of Skin Materials of Civil Airplane Structures. In: Bos, M.J. (eds) ICAF 2009, Bridging the Gap between Theory and Operational Practice. Springer, Dordrecht. https://doi.org/10.1007/978-90-481-2746-7_38
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DOI: https://doi.org/10.1007/978-90-481-2746-7_38
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