Fatigue crack growth failure and lifing analyses for metallic aircraft structures and components

Numerical modeling and simulation of fatigue crack growth rate due to cyclic loading on doubler structure fuselage skin station number 360-380 stringer 6L-7L Boeing 737-900 extended range aircraft

Hydrogen absorption induced slow crack growth in austenitic stainless steels for petrochemical pressure vessel industries

Studi pengaruh posisi semi elliptical crack pada pelat berpenegar dengan profil T dan Y terhadap kekuatan fatik = Study of the influence of semi elliptical crack positions on stiffened plates with T and Y profiles in respect to fatigue strength

Studi tentang prediksi pertumbuhan retak dengan menggunakan konsep tingkat pelepasan energi = Study on crack growth prediction by using strain release rate energy concept