PSI - Issue 21

Hande Yavuz / Procedia Structural Integrity 21 (2019) 112–119 H. Yavuz/Structural Integrity Procedia 00 (2019) 000 – 000

119

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Laulusa, A., Bauchau, O.A., Choi, J.Y., Tan, V.B.C., Li, L., 2006. Evaluation of Some Shear Deformable Shell Elements, International Journal of Solids and Structures 43, 5033 – 5044. Martin, R.H., 1995. Composite Materials: Fatigue and Fracture, STP1230, ASTM, Philadelphia, PA, USA. MATLAB vR2015a, The Mathworks Inc., Massachusetts, MA, USA. Monroy Aceves, C, Skordos, A.A., Sutcliffe, M.P.F., 2008. Design Selection Methodology for Composite Structures, Materials & Design 29, 418 – 426. Schijve, J., 1994. Fatigue of Aircraft Materials and Structures. International Journal of Fatigue 16, 21 – 32. Singh, V., Sharma, S.K., 2015. Fuel Consumption in Air Transport: A Review, Classification, Critique, Simple Meta-Analysis, and Future Research Implications, European Transport Research Review 7:12, 1 – 24. Wanhill, R.J.H., 2018. Fatigue Requirements for Aircraft Structures, in “ Aircraft Sustainment and Repair ” i n: Jones, R., Baker, A., Matthews, N., Champagne, V. (Eds.). Butterworth-Heinemann, Elsevier, Cambridge, MA, USA, pp. 17 – 40. Witcomb, J.D., 1988. Composite Materials: Testing and Design, STP 972, ASTM, Philadelphia, PA, USA. Zhu, F., Qiu, T., 1991. Experimental Investigation on Flutter Characteristics of Composite Torsion-Box, Acta Aeronautica et Astrosinica 12, 550 – 553.