| Laboratorio aeroelasticità dei rotori
(objectives)
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. FURTHERMORE, VIBRATION AND NOISE INDUCED BY ROTOR AEROELASTIC RESPONSE, WHICH ARE IMPORTANT ISSUES DEALT WITH BY MODERN HELICOPTER DESIGN, ARE DESCRIBED AND THEIR MDELLING IS BRIEFLY OUTLINED.
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Code
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20810045 |
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Language
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ITA |
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Type of certificate
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Competence
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Credits
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6
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Scientific Disciplinary Sector Code
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ING-IND/04
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Contact Hours
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-
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Laboratory Hours
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36
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Type of Activity
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Elective activities
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Teacher
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GENNARETTI MASSIMO
(syllabus)
rotor blades dynamics, rotor aerodynamics, dynamics-aerodynamics coupling, methods for analysis of vibratory loads and stability
(reference books)
M. Gennaretti, Fundamentals of aeroelasticity, Springer Nature, 2024.
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Dates of beginning and end of teaching activities
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From to |
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Delivery mode
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Traditional
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Attendance
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not mandatory
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Evaluation methods
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Written test
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Università Roma Tre