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METHODS OF THE APPROXIMATE ESTIMATIONS OF FATIGUE DURABILITY OF COMPOSITE AIRFRAME COMPONENT TYPICAL ELEMENTS

Abstract

Methods of the approximate estimations of fatigue durability of composite airframe component typical elements which can be recommended for application at the stage of outline designing of the airplane are generated and presented.

About the Author

V. E. Strizhius
ЗАО «АэроКомпозит»
Russian Federation


References

1. Whitehead R.S.; Northrop Corporation - Qualification of Primary Aircraft Structures - 14° ICAF symposium, 1987.

2. Стрижиус В.Е. Современные теории усталости элементов композитных авиаконструкций // Общероссийский научно-технический журнал «Полет». - 2013. - № 4. - С. 11-19.

3. Стрижиус В.Е. Методы расчета усталостной долговечности элементов авиаконструкций: справочное пособие. - М: Машиностроение, 2012. - 272 с.

4. Goranson Ulf G. Damage Tolerance Theory and Practice. Moscow Aeronautical University. September 8, 1997. Moscow, Russia.

5. Goranson Ulf G., Hall J., Maclin J.R., Watanabe R.T. Long Life Damage Tolerant Jet Transport Structures. American Society for Testing and Materials. Fatigue and Fracture Committees. Symposium on “Design of Fatigue and Fracture Resistant Structures”. Bal Harbour, Florida. November 10-11, 1980.

6. Tomblin J. and Seneviratne W. Determining the Fatigue Life of Composite Aircraft Structures Using Life and Load-Enhancement Factors. Report DOT/FAA/AR-10/6, June 2011.


Review

For citations:


Strizhius V.E. METHODS OF THE APPROXIMATE ESTIMATIONS OF FATIGUE DURABILITY OF COMPOSITE AIRFRAME COMPONENT TYPICAL ELEMENTS. Civil Aviation High Technologies. 2015;(211):23-28. (In Russ.)

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ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)