Thermal stress analysis of electrothermal anti-ice system embedded in helicopter composite rotor blade undergoing vibratory load
thermal stress dynamic stress progressive fatigue damage properties composite rotor blade electrothermal anti-ice system helicopter
Dong-dong CAO Yu LIU Yong LIU
Shanghai Engineering Center for Microsatellites,Shanghai 201203,China Science and Technology on Rotorcraft Aeromechanics Laboratory,Nanjing University of Aeronautics and
国际会议
10th International Congress on Thermal Stresses(第十届国际热应力大会(TS2013))
南京
英文
1-5
2013-05-31(万方平台首次上网日期,不代表论文的发表时间)