FUNDAMENTALS OF AERONAUTICS
(objectives)
KNOWLEDGE OF THE DIFFERENT TYPE OF AIRCRAFT ARCHITECTURE, OF THE ROLE AND PRINCIPLE OF OPERATION OF THE MAIN AIRCRAFT COMPONENTS FOR FLIGHT PURPOSES; CAPABILITY OF STUDY OF THE AIRCRAFT AS A MATERIAL POINT, FOR ANALYSIS OF PERFORMANCE AND IDENTIFICATION OF CORRESPONDING INFLUENCING PARAMETERS; KNOWLEDGE OF THE MAIN OPERATING CONDITIONS. INTRODUCTION OF SOME METHODOLOGIES FOR MATHEMATICAL MODELLING AND SIMULATION TYPICALLY USED IN AERONAUTICAL ENGINEERING, AND THEIR UTILIZATION.
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Code
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20810096 |
Language
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ITA |
Type of certificate
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Profit certificate
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Credits
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9
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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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72
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Type of Activity
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Core compulsory activities
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Teacher
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BURGHIGNOLI LORENZO
(syllabus)
Aircraft components and their role in flight. Elements of steady aerodynamics of fixed wings: lift and drag coefficients, polar curve of the aircraft; aerodynamic efficiency; finite wings. Dynamics of vehicle as a material point. Fixed-wing aircraft performance: power curve, range and endurance; climb performance, ceiling. Glide performance and climb hodograph. Load factor: steady turn, flare maneuver, gust response. V-n diagram, gust envelope and flight envelope. Take off and landing performance.
Nonlinear algebraic equation solution: iterative methods; Newton-Raphson method. Methods for the solution of ordinary differential equation systems in time domain: first-order form and solution through: (i) eigenvector method, (ii) reference base change, (iii) integration by exponential matrix form. Fourier series, Fourier transform, Laplace transform, transfer function, impulsive, indicial and harmonic response. Linear differential operators: eigenfunctions and eigenfunction method for the solution of systems of partial differential equations. Methods of Galerkin and Rayleigh-Ritz. Calculus of variation: functional and Euler-Lagrange equations; trasversality conditions; the brachistochrone problem; Riccati equation for the optimal control method.
(reference books)
Lecture notes provided by the teacher.
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Dates of beginning and end of teaching activities
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From 19/09/2022 to 23/12/2022 |
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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Oral exam
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Teacher
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GENNARETTI MASSIMO
(syllabus)
Aircraft components and their role in flight. Elements of steady aerodynamics of fixed wings: lift and drag coefficients, polar curve of the aircraft; aerodynamic efficiency; finite wings. Dynamics of vehicle as a material point. Fixed-wing aircraft performance: power curve, range and endurance; climb performance, ceiling. Glide performance and climb hodograph. Load factor: steady turn, flare maneuver, gust response. V-n diagram, gust envelope and flight envelope. Take off and landing performance.
Nonlinear algebraic equation solution: iterative methods; Newton-Raphson method. Methods for the solution of ordinary differential equation systems in time domain: first-order form and solution through: (i) eigenvector method, (ii) reference base change, (iii) integration by exponential matrix form. Fourier series, Fourier transform, Laplace transform, transfer function, impulsive, indicial and harmonic response. Linear differential operators: eigenfunctions and eigenfunction method for the solution of systems of partial differential equations. Methods of Galerkin and Rayleigh-Ritz. Calculus of variation: functional and Euler-Lagrange equations; trasversality conditions; the brachistochrone problem; Riccati equation for the optimal control method.
(reference books)
Lecture notes provided by the teacher.
|
Dates of beginning and end of teaching activities
|
From 19/09/2022 to 23/12/2022 |
Delivery mode
|
Traditional
|
Attendance
|
not mandatory
|
Evaluation methods
|
Oral exam
|
|
|