[1] Gerard R. Minimum Weight Analysis of Compression Structures [M]. New York:New York University Press, 1956.
[2] Khalid M Tahir, ZHANG Xing. Analysis of shear stress distribution in honeycomb aircraft wing structure subjected to(s t) toque[J]. Chinese Journal of Aeronautics, 1997,10(3):182-187.
[3] Khalid M Tahir. The methods of honeycomb structure mechanics and fatigue-damage mechanics[D]. Beijing: Beijing University of Aeronautics and Astronautics, 1998,10-34.
[4] ZHANG Ying-shi, ZHANG Xing. Analytical solution of restrained torsional stresses and displacement for rectangular-section box bar with honeycomb core[J]. Applied Mathematics and Mechanics(English Edition), 2004,25(7): 779-785.
[5] Vlasov V Z. Thin-Walled Elastic Beam[M]. 2nd Ed. Jerasalem:Israel Prog for Scientific Translation, 1961.
[6] von Karman T H, CHIEN Wei-zang. Torsion with variable twist[J]. Journal of the Aeronautical Science, 1946,15(10) :503-511.
[7] Murray N W. Introduction to the Theory of Thin-Walled Structure [M]. Oxford: Clarendon Press,1984.
[8] Hadji Argjris J, Dunne P C. The general theory of cylindrical and conical tubes under torsion and bending loads [J]. The Journal of the Royal Aeronautical Society, 1947,51: 434,441,443. |