LI Gang1,HE Jun-yong2(1.School of First Aviation Air Force,Xingyang 464000,China;2.Beijing University of Aeronautics & Astronautics,Beijing 100083,China)
Abstract：The estimate method of vibrational stress of bladed-disk is given.The vibrational stress of harmonious bladed-disk assemblies under design rotational speed by pneumatic force is calculated firstly.Then the vibrational characters are researched.And its vib
李罡; 何俊勇. 叶盘结构振动应力数值预测方法研究[J]. 南昌大学学报（工科版）, 2007, 29(01): 1-.
LI Gang1,HE Jun-yong2(1.School of First Aviation Air Force,Xingyang 464000,China;2.Beijing University of Aeronautics & Astronautics,Beijing 100083,China). . , 2007, 29(01): 1-.
2007, Vol. 29 