STUDENTS ARE INTRODUCED TO THE METHODOLOGIES ADOPTED FOR THE HELICOPTER FLIGHT MECHANICS ANALYSIS, WHICH IS DOMINATED BY MAIN ROTOR BEHAVIOUR. IN PARTICULAR, PHYSICAL PHENOMENA INVOLVED IN ROTOR AEROELASTICITY AND THE MATHEMATICAL MODEL SUITABLE FOR THEIR DESCRIPTION ARE DESCRIBED.
teacher profile teaching materials
Mutuazione: 20810045 Laboratorio aeroelasticità dei rotori in Ingegneria Aerospaziale LM-20 R GENNARETTI MASSIMO
Programme
rotor blades dynamics, rotor aerodynamics, dynamics-aerodynamics coupling, methods for analysis of vibratory loads and stabilityCore Documentation
M. Gennaretti, Fundamentals of aeroelasticity, Springer Nature, 2024.Attendance
optionalType of evaluation
presentation of the results of an assigned exercise