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STEVAN MAKSIMOVIĆ

ID	Paper title	Created
3567	RESIDUAL LIFE EVALUATION OF A THREADED ROUND BAR WITH SURFACE CRACK UNDER CYCLIC LOADING	13.05.2015.
3566	FATIGUE STRENGTH SIMULATION OF AIRCRAFT LUG	13.05.2015.
3023	Fatigue Strength Simulation of Damaged Lug	03.03.2015.
3021	Residual Life Modeling of Structural Component with Surface Crack	03.03.2015.
3001	FATIGUE LIFE ESTIMATION OF AIRCRAFT STRUCTURAL COMPONENTS WITH SURFACE CRACKS UNDER LOAD SPECTRUM	02.03.2015.
1861	ANALYSIS OF AICRAFT STRUCTURES WITH RESPECTS TO FATIGUE AND FRACTURE MECHANICS	15.01.2013.
1860	Strength Analysis of Damaged Structural Components	15.01.2013.
547	SOME ASPECTS TO DESIGN OF AIRCRAFT STRUCTURES WITH RESPECTS TO FATIGUE AND FRACTURE MECHANICS	26.04.2011.
163	Fatigue Life Estimation of Cracked Structural Components	15.02.2011.
162	SOME ASPECTS TO DESIGN OF AIRCRAFT STRUCTURES WITH RESPECTS TO FATIGUE AND FRACTURE MECHANICS	15.02.2011.
156	CRACK INITIATION LIFE OF NOTCHED METALLIC PARTS EXPOSED TO LOW CYCLE FATIGUE	15.02.2011.

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