Buckling analysis of airframe jointed panel under combined loading

• Autorzy: Li X. , Jia D. , Meng C.

Identyfikatory

DOI

10.2478/ijame-2018-0060

• Języki publikacji: EN

Abstrakty

EN

The complicated relationship of the high order static indeterminate structure will lead to a lot of calculation work. The strength analysis of the structure is very difficult. In aircraft design phase, a structural simplified method should be used to model the load characteristics of the structure. In the paper, the buckling analysis of airframe jointed panel is investigated under combined loading and the effect of jointed position to buckling load is also presented. For the buckling analysis of special joined structure, one new method which is better than traditional methods is described.

Słowa kluczowe

EN

strength; buckling analysis; jointed panel; combined loading

PL

wytrzymałość; wyboczenie; obciążenie

• Wydawca: Oficyna Wydawnicza Uniwersytetu Zielonogórskiego
• Czasopismo: International Journal of Applied Mechanics and Engineering
• Rocznik: 2018
• Tom: Vol. 23, no. 4
• Strony: 1035--1042
• Opis fizyczny: Bibliogr. 10 poz., rys., tab.

Twórcy

autor

Li X.

• Research and Development Center AVIC SAC Commercial Aircraft Company Ltd. Shenyang 110179, CHINA

autor

Jia D.

• Research and Development Center AVIC SAC Commercial Aircraft Company Ltd. Shenyang 110179, CHINA

autor

Meng C.

• School of Science, Shenyang Aerospace University Shenyang 110136, CHINA

Bibliografia

• [1] Gerard G. and Becker H. (1957): Handbook of structural stability. Part 1 buckling of flat plates. – NACA Technical Note 3781.
• [2] Timoshenko and Gere (1963): Theory of Elastic Stability. – USA: McGraw-Hill International Book Company.
• [3] Megson T.H.G. (2013): Introduction to Aircraft Structural Analysis. – Butterworth-Heinemann.
• [4] Huston R. and Josephs H. (2009): Practical stress analysis in engineering design. – CRC Press.
• [5] Liu B., Zhang B. and Sun Q. (2011): Study on overall buckling strength of stiffened panels. – Journal of Mechanical Science and Technology for Aerospace Engineering, vol.30, No.12, pp.1977-1980.
• [6] Beerhorst M. and Seibel M. (2011): Buckling behavior of an orthotropic plate strip under combined compression and shear. – Journal of Aircraft, vol.48, No.4, pp.1360-1367.
• [7] Engineering Sciences Data Unit (1949): Initial buckling of flat plates under compression, bending and shear. – ESDU 02.04.05.
• [8] Bruhn E.F. (1973): Analysis and Design of Flight Vehicle Structures. – USA: Jacobs Publishing, Inc.
• [9] Niu C.Y. (1999): Airframe Stress Analysis and Sizing. – Hong Kong Conmilit Press Ltd.
• [10] Ma A.J. and Zhou C.Y. (2005): Wang X. Patran and Nastran finite element analysis professional tutorial. – Beijing: Tsinghua University Press.

Uwagi

PL

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019)