03.1 - Materials issues, Fatigue and Damage Tolerance
DETERMINATION OF DESIGN ALLOWABLES FOR AIRCRAFT COMPOSITE STRUCTURES
J.Y. Choung¹, J.W. Kim¹, I.H. Hwang¹; ¹Korea Aerospace Research Institute, South Korea
This study shows the aerospace material allowables of composite materials by using CMH-17 STATS software which has been developed by National Center for Advanced Materials Performance(NCAMP). The results of this study have been utilized for the domestic composite material qualification database system and material characteristics database sharing system.