论文撰写等能力得到锻炼。 The structural design is an important part for the research and development of aircraft. It aims to produce the lightest structure scheme which satisfies the safety, reliability and economy. To achieve this goal, it needs for the design of load transferring in structures, stress analysis, judgement of structural failure, and so on. Structural Mechanics is to develop the knowledge and ability required for these jobs. It is a professional basic course for the major of aircraft design. The prerequisite courses are Material Mechanics and Theoretical Mechanics The main contents of this course include basic elasticity, stress calculation of typical structural parts, bending of thin plate, stability of thin-walled structure, *课程简介 external load of aircraft, thin-walled beam theory, and the internal force (Description) calculation of the spar, wing and fuselage. A curriculum design is required at the end of semester The core purpose of this course is to equip students with the basic capabilities of aircraft structural modeling and calculation. Through the studying of this course students can understand the requirements of aircraft structural design and process mechanical characteristics of aircraft structure, the method to simplifying and calculating. They are going to have the ability to complete the preliminary design, the stress analysis and the instability determination on the aircraft structural component. Through the curriculum design, they will also get exercises on teamwork, expression, references organization and report writing 课程教学大纲( course syllabus) 1了解飞行器结构设计的流程。(A52) 2学习弹性力学基本理论,应用弹性力学知识求解典型结构元件的应力、应变,了解 结构应变测量方法。(A5.21,A52.2,A52.3) 3学习薄板弯曲理论,掌握薄板弯曲问题的理论解。(A5.2.1,A5.2.2,A5.2.3) *学习目标 4学习薄壁稳定性理论,掌握飞行器结构中典型的薄壁稳定性计算方法。(A5.2.1, A52.2,A52.3) Out 5学习薄壁梁理论,掌握翼梁、机翼、机身等典型飞行器部件内力的建模和计算方法。 (A521,A5.2.2,A523) 6根据初始设计要求完成飞行器结构部件的构型设计、应力分析和稳定性计算,并撰 写设计报告。(A521,A522,A523,B9,B11,B12)论文撰写等能力得到锻炼。 *课程简介 （Description） The structural design is an important part for the research and development of aircraft. It aims to produce the lightest structure scheme which satisfies the safety, reliability and economy. To achieve this goal, it needs for the design of load transferring in structures, stress analysis, judgement of structural failure, and so on. Structural Mechanics is to develop the knowledge and ability required for these jobs. It is a professional basic course for the major of aircraft design. The prerequisite courses are Material Mechanics and Theoretical Mechanics. The main contents of this course include basic elasticity, stress calculation of typical structural parts, bending of thin plate, stability of thin-walled structure, external load of aircraft, thin-walled beam theory, and the internal force calculation of the spar, wing and fuselage. A curriculum design is required at the end of semester. The core purpose of this course is to equip students with the basic capabilities of aircraft structural modeling and calculation. Through the studying of this course students can understand the requirements of aircraft structural design and process, mechanical characteristics of aircraft structure, the method to simplifying and calculating. They are going to have the ability to complete the preliminary design, the stress analysis and the instability determination on the aircraft structural component. Through the curriculum design, they will also get exercises on teamwork, expression, references organization and report writing. 课程教学大纲（course syllabus） *学习目标 (Learning Outcomes) 1 了解飞行器结构设计的流程。（A5.2） 2 学习弹性力学基本理论，应用弹性力学知识求解典型结构元件的应力、应变，了解 结构应变测量方法。（A5.2.1，A5.2.2，A5.2.3） 3 学习薄板弯曲理论，掌握薄板弯曲问题的理论解。（A5.2.1，A5.2.2，A5.2.3） 4 学习薄壁稳定性理论，掌握飞行器结构中典型的薄壁稳定性计算方法。（A5.2.1， A5.2.2，A5.2.3） 5 学习薄壁梁理论，掌握翼梁、机翼、机身等典型飞行器部件内力的建模和计算方法。 （A5.2.1，A5.2.2，A5.2.3） 6 根据初始设计要求完成飞行器结构部件的构型设计、应力分析和稳定性计算，并撰 写设计报告。（A5.2.1，A5.2.2，A5.2.3，B9，B11，B12）