Academic year2016/17
CourseAEROSPACE ENGINEERING
Code165II
Credits6
PeriodSemester 1
LanguageItalian
| Modules | Area | Type | Hours | Teacher(s) |
| TERMODINAMICA APPLICATA | ING-IND/10 | LEZIONI | 60 | |
Programma non disponibile nella lingua selezionata
Knowledge
The student who completes this academic course will be to show a good knowledge of the thermodynamic science and heat transfer applied to the aerospace engineering in particular. A wide knowledge of thermodynamic physical transformations applied to the engineering device will be acquired. The student will be able to model the main thermodynamic systems and to control the thermal physical parameters which characterize the evolution of the several thermal engineering process. Device as aeromotive and automotive engines, rockets, propellent containers, thermal and nuclear electrical plant, freezing systems and heat pumps will be analysed and studied. The student will be able to sole alone basic heat transfer problems.
Assessment criteria of knowledge
- The student will be assessed on his/her demonstrated ability to discuss the main course contents using the appropriate terminology.
- The student must shown a good capability to connect different sections
of the subject between them.
- During the final oral exam the student must be able to solve practise exercises
on technical problems analysed during the course or similar.
- The student must demonstrate the ability to put into practice and to execute, with critical awareness, the activities illustrated or carried out under the guidance of the teacher during the course.
Methods:
Further information:
During the final oral exam will be made three different questions. The first one (the most important 50% of the mark) is devoted to thermodynamic program, the second one (25% about) deals with the nozzle and pressure losses topic and laslty, the third one questions (25%) concerns with heat transfer.
Teaching methods
Delivery: face to face
Learning activities:
- attending lectures
- participation in seminar
- individual study
- Practical
Attendance: Advised
Teaching methods:
Syllabus
This course provides notion about the thermodynamic systems and the main thermodynamic property relations. Furthermore the 1st and 2nd Law of Thermodynamics are formulated and applied, together with the cyclic processes and the definition of thermodynamic engine, refrigerator and heat pump. The main relationship to predict the behavior of ideal gases and real gases, liquid and vapour and solid are shown. Several vapour and combined power cycles are shown together with gas power an refrigerator cycles. Are provided also the main relationships to describe the flow through nozzles and diffusers as well as the correlation to predict the pressure losses in pipes and loops. Lastly the fundamentals of heat transfer are provided.
Bibliography
All the books which are advised are in italian, but the books number 1 and 2 it is possibile to find them also in english version.
1) M.J Moran, H.N. Shapiro, B.R. Munson, D.P.DeWitt, Elementi di Fisica Tecnica per l’ingegneria , McGraw-Hill, 2003.
2)Y.A. Cengel, Termodinamica e Trasmissione del Calore, McGraw-Hill, 1998.
3) E.Latrofa, Fisica Tecnica - Termodinamica, Andrea Vallerini Editore, Pisa, 1994.
4) Cavallini e L. Mattarolo, Termodinamica Applicata, CLEUP, Padova, 1992.
5) C. Bonacina, A. Cavallini e L. Mattarolo, Trasmissione del calore, CLEUP, Padova, 1975.
For practise the references are:
6) E. Latrofa, F. Fantozzi, A. Franco, Esercizi di termodinamica applicata, Andrea Vallerini Ed., Pisa, 2000.
7) Boeche, A. Cavallini e S. Del Giudice, Problemi di Termodinamica Applicata, CLEUP, Padova, 1992.
8) Schaum Electronic Book, Thermodynamics (An interactive electronic book with several programs in Mathcad)
Updated: 14/11/2016 17:27
