- Docente: Elisabetta De Angelis
- Credits: 9
- SSD: ING-IND/06
- Language: Italian
- Moduli: Elisabetta De Angelis (Modulo 1) Stefania Falfari (Modulo 2)
- Teaching Mode: Traditional lectures (Modulo 1) Traditional lectures (Modulo 2)
- Campus: Forli
- Corso: First cycle degree programme (L) in Aerospace Engineering (cod. 8263)
Learning outcomes
The objective is to give the students the basic information in fluid mechanics and gas dynamics required to understand the behavior of all the airbreathing propulsion systems.
Course contents
Module 1: Fluid Dynamics
Introduction to tensorial analysis. Eulerian/Lagragian description. Reynolds transport theorem. Conservation of Mass. Conservation of Momentum. Conservation of Energy. Constitutive relations for Newtonian and non Newtonian fluids. Entropy balance.
System of equations for fluid mechanics. Non dimesional analysis. Finite difference methods for convection-diffusion. Natural and forced convection. Low Reynolds number flows, Stokes flow. High Reynolds number flows. Euler equations. Irrotational flows: vorticity and circulation. Potential flows.
Boundary layer. Solution methods. Blasius solution.
Outer solutions for compressible flows. Small perturbation approach for subsonic and supersonic flows. Shock equations.
Module 2: Thermodynamic System
Classification of machinery.
Water as a potential fluid: characteristics and Ts and hs
diagrams.
Conservation of mass. Energy conservation: first principle for a
closed system and for an open system (mechanical and thermal).
Entropy and enthalpy.
Ideal gas and ideal fluid: definition, major transformations and
their representation on the Ts, hs diagrams. Work and
efficiency, polytropic and isentropic efficiency for a compression
and an expansion.
Combustion: definition of stoichiometric air, excess air, lower
heating value.
Gas turbine thermodynamic cycle
Generality, Brayton cycle, simple plant configuration and
cycle representation on the diagram Ts. Conditions for the
representability of the cycle in the Ts diagram. Thermodynamic
analysis of gas turbine self-sustaining condition. Assessment of
performance. Condition of maximum useful work and maximum
efficiency.
Regenerative cycle, thermodynamic diagrams, problems and
limitations in employment.
Cycle with separated compression phases (inter-cooling):
Schematic diagram and thermodynamic conditions. Complete
inter-cooling, condition of maximum useful work, problems and
limitations in employment.
Post-combustion cycle: Schematic diagram and thermodynamic
process.
Compression refrigeration cycle
Definition of COP. Cycle at saturated vapor compression
cycle (biphasic with intercooler, dual-separator, dual-separator
with bubbler), biphasic compression cycle with two temperatures of
vaporization. Characteristics of fluids for refrigeration equipment
and their classification.
Applications of refrigeration cycles to liquefaction of hydrogen
and oxygen.
Readings/Bibliography
Lecture notes of Prof. Piva
Sistemi energetici e loro componenti, 2a ed., G. Negri di Montenegro, M. Bianchi, A. Peretto, Pitagora Editrice Bologna
Assessment methods
The final exam will be divided in two different phases:
1) module 1 - written examination followed by
an oral discussion
2) module 2 - oral examination
Office hours
See the website of Elisabetta De Angelis
See the website of Stefania Falfari