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.
|
Code
|
20810096 |
Language
|
ITA |
Type of certificate
|
Profit certificate
|
Credits
|
9
|
Scientific Disciplinary Sector Code
|
ING-IND/04
|
Contact Hours
|
72
|
Type of Activity
|
Core compulsory activities
|
Teacher
|
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.
|
Dates of beginning and end of teaching activities
|
From 18/09/2024 to 23/12/2024 |
Delivery mode
|
Traditional
|
Attendance
|
not mandatory
|
Evaluation methods
|
Oral exam
|
Teacher
|
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 18/09/2024 to 23/12/2024 |
Delivery mode
|
Traditional
|
Attendance
|
not mandatory
|
Evaluation methods
|
Oral exam
|
|
|