Mathematical Models and Methods for Calculating the Stress-Strain State of Aircraft Panels from Composite Materials Taking into Account the Production Technology

Author:

Gavva L. M.,Firsanov V. V.

Publisher

Allerton Press

Subject

General Physics and Astronomy,Mechanics of Materials

Reference20 articles.

1. I. F. Obraztsov, O. S. Sirotkin, and V. B. Litvinov, “Integral constructions from composite materials and prospects of their application,” Konstruktsii Kompozits. Mater., No. 2, 78–84 (2000).

2. A. B. Akhmetov, “Qualitative algorithm of theories of plates made of composite materials,” Probl. Mekh., No. 1, 81–84 (2011).

3. Yu. V. Nemirovsky and G. L. Gorynin, “Method of stiffnesible functions in calculation problems of multilayeral beams and plates,” Vestn. Nizhegorodsk. Univ. Lobachevskogo 4 (4), 1654–1656 (2011).

4. E. Carrera, “Developments, ideas, and evaluations based upon Reissner’s mixed variational theorem in the modelling of multilayered plates and shells,” Appl. Mech. Rev. 54 (4), 301–329 (2001).

5. E. Carrera and L. Demasi, “Two benchmarks to assess two-dimensional theories of sandwich, composite plates,” AIAA J. 41 (7), 1356–1362 (2003).

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