Teaching
Course in the Second Year (first semester) of the second level degree on Aeronautical Engineering
Credits number: 6
Learning Objectives: The course gives the foundations of the linear theory of the Aeroelasticity (linearly elastic solids in linearized potential flows). Thus, the modeling of the aeroelasticity of fixed wing is comprehensively described and the consequent stability and response (flutter, divergence, gust response, control-surface response, aileron effectiveness and reversal) are faced together with the specific issues due to their numerical implementation. Some general issues on nonlinear aerolasticity are also presented (post- pre-critical behaviors).
Hours of Lesson: 50
Hours of laboratory practice : 10
Hours of personal study : 100
Course attending: not mandatory
Evaluation: written and oral
Course in the First Year (second semester) of the second level degree on Aeronautical Engineering
Credits number: 9
Learning Objectives: The course is designed in order to achieve a fulfilment of the basic preparation in the aeronautical structure field by a study of analitical and numerical methods. A particular attention is devoted to the structural dynamics and structural design of aeronautical structures.
Hours of Lesson: 80
Hours of laboratory practice : 10
Hours of personal study : 135
Course attending: not mandatory
Evaluation: written and oral