CONTINOUS ESTIMATION OF AIRPLANE LOAD-BEARING STRUCTURES FATIGUE
HYPOTHESIS OF LOADS CYCLE REDUCTION TO EQUIVALENT FATIGUE CYCLE
INCREASING IDEA OF EXPLOITATION SAFETY AND RELIABILITY OF THE SHIPS AND OTHER SEA STRUCTURES
REDUCTION A FATIGUE LOAD CYCLE TO EQUIVALENT CYCLE - D-G-D LOAD REDUCTION'S HYPOTHESIS
IDEA OF CONTINUOUS FATIGUE ESTIMATION OF AIRPLANES LIFTING STRUCTURES
NEW LIMIT CURVES OF THE COMPLEX STRESS - STATE FATIGUE STRENGTH