Fatigue life of a carbon fiber composite T-joint under a standard fighter aircraft spectrum load sequence

Autor: Thawre, M.M., Pandey, K.N., Dubey, A., Verma, K.K., Peshwe, D.R., Paretkar, R.K., Jagannathan, N., Manjunatha, C.M.
Zdroj: In Composite Structures 1 September 2015 127:260-266
Databáze: ScienceDirect