Passive Aeroelastic Tailored Wing Ground Vibration Test Using Fixed Base Correction Method
[摘要]
[发布日期] 2019-06-10 [发布机构]
[效力级别] [学科分类] 力学，机械学
[关键词] ACCELEROMETERS;AERODYNAMIC LOADS;AEROELASTICITY;AIRCRAFT DESIGN;CORRECTION;FINITE ELEMENT METHOD;MATHEMATICAL MODELS;RETRACTABLE EQUIPMENT;TEST FACILITIES;WING LOADING;WINGS [时效性]
