COURSE - Università Roma Tre

Degree Course: Aeronautical engineering A.Y. 2016/2017

Expected learning outcomes Syllabus Italian version

FIRST YEAR

First semester

Course	Credits	Scientific Disciplinary Sector Code	Contact Hours	Exercise Hours	Laboratory Hours	Personal Study Hours	Type of Activity	Language
20801740 - AERODYNAMICS (objectives) FUNDAMENTAL CONCEPTS ON AERODYNAMICS OF WINGS AND PROFILES INCLUDING TURBULENCE AND ANALYSIS OF RANDOM SIGNALS. THE COURSE WILL PROVIDE BASIC INSTRUMMENTS FOR AERODYNAMIC DESIGN WITH STANDARD APPROACHES.	9	ING-IND/06	72	-	-	-	Core compulsory activities	ITA
20801741 - AERONAUTICAL CONSTRUCTIONS (objectives) INTRODUCTION TO THE BASIC COMPONENTS OF AERONAUTICAL STRUCTURES: ANALYSIS OF STRESS AND STRAIN. COMPLEX AERONAUTICAL STRUCTURES WITH EMPHASIS ON WING BOX AND FUSELAGE: THEIR MATHEMATICAL MODELING FOR PRELIMINARY DESIGN PURPOSES AND STRUCTURAL INSTABILITY ANALYSIS.	9	ING-IND/04	72	-	-	-	Core compulsory activities	ITA

Second semester

Course	Credits	Scientific Disciplinary Sector Code	Contact Hours	Exercise Hours	Laboratory Hours	Personal Study Hours	Type of Activity	Language
20801830 - FLIGHT DYNAMICS (objectives) EQUATIONS OF MOTION OF THE AERIAL VEHICLE AND ITS PERFORMANCE. MATERIAL POINT AND RIGID BODY STUDIES. CHARACTERISTIC FLIGHT SEGMENTS. STABILITY AND CONTROL.	9	ING-IND/03	72	-	-	-	Core compulsory activities	ITA
20810027 - THERMO-FLUID DYNAMICS FOR PROPULSION SYSTEMS (objectives) FUNDAMENTALS OF COMPRESSIBLE FLOWS IN CHANNELS, INCLUDING NON ISENTROPIC RAYLEIGH AND FANNO FLOWS. OBLIQUE SHOCK WAVES. PRANDTL MEYER EXPANSIONS. COMPRESSIBLE POTENTIAL FLOWS AND SMALL PERTURBATION THEORIES FOR SUBSONIC AND SUPERSONIC FLOWS. SUPERSONIC PROFILES AND WINGS. THERMODYNAMIC DESCRIPTION OF AIR-BREATHING ENGINES AND PROPELLERS. BLADE ELEMENT THEORY.	9	ING-IND/08	72	-	-	-	Related or supplementary learning activities	ITA
20810083 - MODELING IN AERONAUTICS (objectives) TO FAMILIARIZE THE STUDENT WITH THE METHODOLOGIES FOR MODELLING AND SIMULATION TYPICALLY USED IN AERONAUTICAL ENGINEERING AND THEIR UTILIZATION. MODELLING COMPRISES THOSE MATHEMATICAL MODELS (SUCH AS THE MODAL APPROACH) THAT ARE QUITE EFFICIENT IN PROVIDING AN APPROXIMATION OF THE PHYSICAL PHENOMENON, ALONG WITH THE CORRESPONDING SOLUTION METHODOLOGIES. ON THE OTHER HAND, SIMULATION REFERS TO THOSE NUMERICAL METHODS (SUCH AS THE FINITE ELEMENT METHODS) THAT DESCRIBE THE PHYSICAL PHENOMENON IN GREATER DETAIL.	9	ING-IND/04	72	-	-	-	Core compulsory activities	ITA

SECOND YEAR

First semester

Course

Credits

Scientific Disciplinary Sector Code

Contact Hours

Exercise Hours

Laboratory Hours

Personal Study Hours

Type of Activity

Language

20801826 - AEROELASTICITY (objectives)

ING-IND/04

Core compulsory activities

ITA

20801822 - LABORATORY: AERODYNAMICS AND AEROACOUSTICS (objectives)

ING-IND/06

Core compulsory activities

ITA

20802034 - Additional skills

Other activities

ITA

Optional Group: comune Orientamento unico AD OBBLIGATORIE AFFINI - (show)

20801744 - MATERIALS TECHNOLOGY FOR AERONAUTICS	Also available in another semester or year
20801817 - ADVANCED AUTOMATIC CONTROLS STUDIES (objectives) STATE SPACE: INPUT-STATE REPRESENTATIONS, INTERCONNECTION OF SYSTEMS, TRANSITION MATRIX, EXPONENTIAL OF A MATRIX, FROM TRANSFER FUNCTION TO STATE SPACE AND VICE-VERSA, COORDINATE TRANSFORMATION, EGINEVALUES, MODAL ANALYSIS, STRUCTURAL PROPERTIES, ASYMPTOTIC OBSERVER, EIGENVALUES ASSIGNEMENT, SEMPARATION PRINCIPLE, OUTPUR REGULATION, OPTIMAL CONTROL. DISCETE TIME SYSTEMS: DISCRETE IMPLEMENTATION OF FEEDBACK CONTROL SYSTEM. HARDWARE CHARACTERISTICS, D/A AND A/D CONVERSION. SAMPLING AND RECONSTRUCTION, SHANNON THEOREM. DIFFERENCE EQUATIONS, Z TRANSFORM, MODES, STABILITY. APPROXIMATE METHODS. SYNTHESIS OF CONTROL SYSTEMS.
20801817-1 - COMPLEMENTI DI CONTROLLI AUTOMATICI MODULO I (objectives) STATE SPACE: INPUT-STATE REPRESENTATIONS, INTERCONNECTION OF SYSTEMS, TRANSITION MATRIX, EXPONENTIAL OF A MATRIX, FROM TRANSFER FUNCTION TO STATE SPACE AND VICE-VERSA, COORDINATE TRANSFORMATION, EGINEVALUES, MODAL ANALYSIS, STRUCTURAL PROPERTIES, ASYMPTOTIC OBSERVER, EIGENVALUES ASSIGNEMENT, SEMPARATION PRINCIPLE, OUTPUR REGULATION, OPTIMAL CONTROL. DISCETE TIME SYSTEMS: DISCRETE IMPLEMENTATION OF FEEDBACK CONTROL SYSTEM. HARDWARE CHARACTERISTICS, D/A AND A/D CONVERSION. SAMPLING AND RECONSTRUCTION, SHANNON THEOREM. DIFFERENCE EQUATIONS, Z TRANSFORM, MODES, STABILITY. APPROXIMATE METHODS. SYNTHESIS OF CONTROL SYSTEMS.	6	ING-INF/04	48	-	-	-	Related or supplementary learning activities	ITA
20801817-2 - COMPLEMENTI DI CONTROLLI AUTOMATICI MODULO II (objectives) STATE SPACE: INPUT-STATE REPRESENTATIONS, INTERCONNECTION OF SYSTEMS, TRANSITION MATRIX, EXPONENTIAL OF A MATRIX, FROM TRANSFER FUNCTION TO STATE SPACE AND VICE-VERSA, COORDINATE TRANSFORMATION, EGINEVALUES, MODAL ANALYSIS, STRUCTURAL PROPERTIES, ASYMPTOTIC OBSERVER, EIGENVALUES ASSIGNEMENT, SEMPARATION PRINCIPLE, OUTPUR REGULATION, OPTIMAL CONTROL. DISCETE TIME SYSTEMS: DISCRETE IMPLEMENTATION OF FEEDBACK CONTROL SYSTEM. HARDWARE CHARACTERISTICS, D/A AND A/D CONVERSION. SAMPLING AND RECONSTRUCTION, SHANNON THEOREM. DIFFERENCE EQUATIONS, Z TRANSFORM, MODES, STABILITY. APPROXIMATE METHODS. SYNTHESIS OF CONTROL SYSTEMS.	3	ING-INF/04	24	-	-	-	Related or supplementary learning activities	ITA
20801821 - INTERACTIONS BETWEEN MACHINES AND THE ENVIRONMENT (objectives) ACQUISITION OF BASIC KNOWLEDGE ABOUT POLLUTANTS FORMATION IN POWER PLANT AND MOTOR VEHICLE; ACQUISITION OF TOOLS FOR AIR POLLUTION MODELING. ACQUISITION OF ADVANCED KNOWLEDGE TO ANALYZE SOURCES IN LIGHT OF THEIR POLLUTANTS EMISSIONS; ACQUISITION OF SKILLS NECESSARY TO MEASURE AND CONTROL THE EMISSIONS IN ATMOSPHERE (PRE-COMBUSTION, COMBUSTION AND POST-COMBUSTION CONTROLS).	9	ING-IND/08	72	-	-	-	Related or supplementary learning activities	ITA
20801825 - TURBOMACHINES (objectives) THE AIM OF THE COURSE IS TO PROVIDE STUDENTS WITH PRELIMINARY DESIGN PROCEDURES AND CRITERIA FOR TURBOMACHINES. (FROM GAS, STEAM, AND HYDRAULIC TURBINES TO PUMPS, FANS, BLOWERS AND COMPRESSORS). MOVING FROM PERFORMANCE TARGETS AND SPECIFIC DESIGN BOUNDARY CONDITIONS, THE STUDENT WILL LEARN SOME SIMPLIFIED DESIGN METHODOLOGIES TAKING MATERIAL, MECHANICAL AND THERMAL STRESSES, TRANSONIC FLOW LIMITS AND CAVITATION INTO ACCOUNT. THE OPTIMIZATION OF THE DEGREE OF FREEDOM WILL BE IMPLEMENTED IN THE DESIGN PROCEDURES. THE STUDENT WILL BE ABLE TO ANALYSE MACHINE PERFORMANCE ONCE THE MAIN GEOMETRIC QUANTITIES ARE GIVEN.	9	ING-IND/08	72	-	-	-	Related or supplementary learning activities	ITA
20801835 - INTERNAL COMBUSTION ENGINES	Also available in another semester or year
20801838 - OLEODYNAMICS AND PNEUMATICS	9	ING-IND/08	72	-	-	-	Related or supplementary learning activities	ITA

Second semester

Course

Credits

Scientific Disciplinary Sector Code

Contact Hours

Exercise Hours

Laboratory Hours

Personal Study Hours

Type of Activity

Language

20801818 - STRUCTURAL DESIGN OF AIRCRAFT (objectives)

ING-IND/04

Core compulsory activities

ITA

20801816 - ANALYSIS OF AERONAUTICAL STRUCTURES (objectives)

ING-IND/04

Core compulsory activities

ITA

Optional Group: comune Orientamento unico AD OBBLIGATORIE AFFINI - (show)

20801744 - MATERIALS TECHNOLOGY FOR AERONAUTICS (objectives) The objectives of the course “Materials technologies for aeronautical engineering” can be summarized as follows: 1. To provide students with the know-how for the correct and timely selection of materials for the most relevant aeronautical application, even by the use of recently developed software; 2. To provide students with the basic knowledge on structural materials for aeronautics and aerospace, including polymer matrix composites, light alloys, super-alloys for high-temperature applications, advanced ceramics and coatings ()structure-property-process correlations and applications for components in aircrafts); 3. To provide students with the fundamentals of corrosion and wear, with specific reference to the main advanced engineering aspects of such degradation phenomena; 4. To provide students with the most important concepts of surface engineering and the applications to aeronautical and aerospace engineering; 5. To provide students with the fundamental aspects of advanced microstructural characterization of materials for aeronautics and aerospace, including optical and electron microscopy, focused ion beam microscopy); 6. To provide students with the main know-how on micro- and nano-mechanical characterization of materials for aeronautics (including micro-and nano-indentation and atomic force microscopy). Students will acquire required knowledge and expertise for (1) the proper selection of suitable materials on the basis of design specifications, (2) understanding the main processes and heat treatments required for microstructural control of advanced materials for aeronautics and aerospace, (3) understanding the corrosion and wear mechanisms in aerospace materials, (4) understanding the main applications and concepts of recent surface engineering and coating technologies.	9	ING-IND/22	72	-	-	-	Related or supplementary learning activities	ITA
20801817 - ADVANCED AUTOMATIC CONTROLS STUDIES (objectives) STATE SPACE: INPUT-STATE REPRESENTATIONS, INTERCONNECTION OF SYSTEMS, TRANSITION MATRIX, EXPONENTIAL OF A MATRIX, FROM TRANSFER FUNCTION TO STATE SPACE AND VICE-VERSA, COORDINATE TRANSFORMATION, EGINEVALUES, MODAL ANALYSIS, STRUCTURAL PROPERTIES, ASYMPTOTIC OBSERVER, EIGENVALUES ASSIGNEMENT, SEMPARATION PRINCIPLE, OUTPUR REGULATION, OPTIMAL CONTROL. DISCETE TIME SYSTEMS: DISCRETE IMPLEMENTATION OF FEEDBACK CONTROL SYSTEM. HARDWARE CHARACTERISTICS, D/A AND A/D CONVERSION. SAMPLING AND RECONSTRUCTION, SHANNON THEOREM. DIFFERENCE EQUATIONS, Z TRANSFORM, MODES, STABILITY. APPROXIMATE METHODS. SYNTHESIS OF CONTROL SYSTEMS.
20801817-1 - COMPLEMENTI DI CONTROLLI AUTOMATICI MODULO I	Also available in another semester or year
20801817-2 - COMPLEMENTI DI CONTROLLI AUTOMATICI MODULO II	Also available in another semester or year
20801821 - INTERACTIONS BETWEEN MACHINES AND THE ENVIRONMENT	Also available in another semester or year
20801825 - TURBOMACHINES	Also available in another semester or year
20801835 - INTERNAL COMBUSTION ENGINES (objectives) ACQUISITION OF TOOLS FOR ANALYZING RECIPROCATING INTERNAL COMBUSTION ENGINES PERFORMANCES, SPARK IGNITION AND DIESEL ONES, FOR USE IN BOTH INDUSTRIAL, AND TRANSPORT SECTORS. REFINEMENT OF KNOWLEDGE ON OPERATIONAL ISSUES RELATED TO THE THERMO-FLUID DYNAMICS OF RECIPROCATING ENGINES, COMBUSTION, POLLUTION CONTROL AND MANAGEMENT OF ENGINE POWER TRAIN ACQUISITION OF TOOLS FOR THE ANALYSIS OF FUNCTIONAL CHARACTERISTICS OF PLANTS WITH GAS TURBINE ENGINES FOR BOTH THE INDUSTRY AND FOR THE AVIATION, MARINE AND TERRESTRIAL PROPULSION. ACQUISITION OF OPERATIONAL SKILLS NECESSARY FOR PROFESSIONAL ACTIVITY IN PLANTS WITH GAS TURBINES.	9	ING-IND/08	72	-	-	-	Related or supplementary learning activities	ITA
20801838 - OLEODYNAMICS AND PNEUMATICS	Also available in another semester or year

20801832 - FINAL EXAM

Final examination and foreign language test

ITA

22902343 - STUDENT'S CHOICE OF COURSE

Elective activities

ITA

TOTAL

120

Università Roma Tre

Degree Course: Aeronautical engineering A.Y. 2016/2017

Expected learning outcomes Syllabus Italian version

Autonomia di giudizio

Abilità comunicative

Capacità di apprendimento

Requisiti di ammissione

Prova finale

Orientamento in ingresso

Il Corso di Studio in breve