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.
scheda docente
materiale didattico
Mutuazione: 20810045 Laboratorio aeroelasticità dei rotori in Ingegneria Aerospaziale LM-20 R GENNARETTI MASSIMO
Programma
rotor blades dynamics, rotor aerodynamics, dynamics-aerodynamics coupling, methods for analysis of vibratory loads and stabilityTesti Adottati
M. Gennaretti, Fundamentals of aeroelasticity, Springer Nature, 2024.Modalità Frequenza
optionalModalità Valutazione
presentation of the results of an assigned exercise