摘要
以《军用飞机强度和刚度规范—总则》(GJB67.1-85)为标准,以《军用飞机强度和刚度规范—飞行载荷》(GJB67.2-85)、《军用飞机强度和刚度规范—其它载荷》(GJB67.3-85)为指南,结合型号研制,提出一套军用飞机飞行载荷计算方法,并开发了“军用飞机飞行载荷计算分析软件”,该方法及软件在型号研制中得到应用。
Taking 《Military Aircraft Strength and Rigidity Specification- General》 （GJB67.1 -85） as standard, and 《Military Aircraft Strength and Rigidity Specification-Flight Loads》 （GJB67.2- 85） and 《Military Aircraft Strength and Rigidity Specification - Other Loads》 （ GJB67.3 - 85） as guidance, this paper describes a set of calculation method for military aircraft flight loads in combining with the development of a version of aircraft, and has developed ＂ Calculation and Analysis Software of Military Aircraft Flight Loads＂, both of which have been applied in the development of this version of aircraft.
出处
《空气动力学学报》
EI
CSCD
北大核心
2006年第2期238-242,共5页
Acta Aerodynamica Sinica
关键词
飞行载荷
惯性载荷
计算方法
动态平衡
载荷包线
flight load
inertial load
calculation method
dynamic balancing
load envnlope
