HYPOTHESIS OF LOADS CYCLE REDUCTION TO EQUIVALENT FATIGUE CYCLE
CONTINOUS ESTIMATION OF AIRPLANE LOAD-BEARING STRUCTURES FATIGUE
IDEA OF CONTINUOUS FATIGUE ESTIMATION OF AIRPLANES LIFTING STRUCTURES
REDUCTION A FATIGUE LOAD CYCLE TO EQUIVALENT CYCLE - D-G-D LOAD REDUCTION'S HYPOTHESIS
NEW LIMIT CURVES OF THE COMPLEX STRESS - STATE FATIGUE STRENGTH
The Conception Of The Continuous Fatigue Estimation Of The Airplanes