Designing and Calculation of Extruded Sections of an Inhomogeneous Composition

Author:

Babaytsev A. V.,Zotov A. A.

Publisher

Pleiades Publishing Ltd

Subject

Metals and Alloys

Reference20 articles.

1. H.-J. Schmidt, “Development of stringers for damage tolerance integral structures,” in Proceedings of EADS Airbus Technology Seminar on Advanced Fuselage Design (Hamburg, 2001).

2. T. Swift, Fracture Analysis of Stiffened Structure, Damage Tolerance of Metallic Structure: Analysis Methods and Application (ASTM STP, 1984).

3. T. Swift, “Fail–safe design requirements and features, regulatory requirements,” in Proceedings of International Air and Space Symposium and Exposition: The Next 100 Years (Ohio, 2003), p. 2783.

4. U. G. Goranson, “Damage tolerance. Facts and fiction. 14th Plantema Memorial Lecture,” in Proceedings of the 17th Symposium of the International Committee on Aeronautical Fatigue (ICAF) (Stockholm, 1993).

5. B. G. Nesterenko and G. I. Nesterenko, “Safe operation of aircraft structures according to strength conditions,” Probl. Mashinostr. Nadezhn. Mashin, No. 1, 76–92 (2013).

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