火箭捆绑机构热力耦合模型修正与虚拟验证方法

贺揆 1，张薇 2，李长龙 2，裴长浩 2

Model updating and virtual verification for launch vehicle strap-on thermal mechanical structures

HE Kui1，ZHANG Wei2，LI Changlong2，PEI Changhao2

振动与冲击 . 2024, (8): 34 -42 .