Development of optical-digital methods for non-destructive testing of aerospace thin-walled shell structures (Review)

Author:

Muravsky L.I.,

Publisher

International Association Welding

Subject

Mechanics of Materials,Control and Systems Engineering

Reference44 articles.

1. 1. Weingarten, V.I., Seide, P., Peterson, J.P. (1968) Buckling of thin-walled circular cylinders (No. NASA SP-8007), NASA.

2. 2. Meyer-Piening, H.R., Farshad, M., Geier, B., Zimmermann, R. (2001) Buckling loads of CFRP composite cylinders under combined axial and torsion loading-experiments and computations. Composite. Structures, 53(4), 427-435. DOI: https://doi.org/10.1016/S0263-8223(01)00053-8

3. 3. Geier, B., Klein, H., Zimmermann, R. (1991) Buckling tests with axially compressed unstiffened cylindrical shells made from CFRP. In: Buckling of Shell Structures, on Land, in the Sea and in the Air. Proc. of Int. Colloq. (Lyon, France), 498-507.

4. 4. Geier B, Singh, G. (1997) Some simple solutions for buckling loads of thin and moderate thick cylindrical shells and panels made of laminated composite material. Aerospace Sci. and Technol., 1(1), 47-63. DOI: https://doi.org/10.1016/ S1270-9638(97)90023-7

5. 5. Hühne, C., Rolfes, R., Tessmer, J. (2005) A new approach for robust design of composite cylindrical shells under axial compression. In: Spacecraft Structures, Materials and Mechanical Testing, 581, 1-8.

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