Please use this identifier to cite or link to this item:
https://er.nau.edu.ua/handle/NAU/37940| Title: | Aircraft engines. Lecture notes (first preliminary edition). Chapter 3. Theoretical dependencies for an ideal gas |
| Authors: | Goncharenko, Andriy Viktorovich |
| Keywords: | aircraft engine piston type engine gas turbine engine thermodynamic cycle thermodynamic process |
| Issue Date: | 1-Mar-2019 |
| Publisher: | National Aviation University |
| Abstract: | An equation that establishes (sets up) the connection between pressure, temperature, and specific volume of a medium of a constant content (composition, compound) is called the thermodynamic equation of state |
| Description: | The equation of (2.6) in space depicts (portrays, shows, represents, describes, illustrates, gives a picture of) a surface, which characterises all possible equilibrium states of a regular (uniform) thermodynamic system. This surface is called the thermodynamic surface or the surface of state. At the thermodynamic surface a certain point corresponds to each state of the system. |
| URI: | http://er.nau.edu.ua/handle/NAU/37940 |
| Appears in Collections: | Aircraft engines |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| A_I_3.pdf | Chapter 3. Theoretical dependencies for an ideal gas | 132.83 kB | Adobe PDF | View/Open |
| References.pdf | References | 255.57 kB | Adobe PDF | View/Open |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.