Please use this identifier to cite or link to this item:
https://er.nau.edu.ua/handle/NAU/37947| Title: | Aircraft engines. Lecture notes (first preliminary edition). Chapter 10. Heat capacities |
| 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| Abstract: | The amount of heat which is necessary to be taken in into a body or withdrawn from it in order to change its temperature in 1 °C is called heat capacity. Heat capacity is calculated by the formula. |
| Description: | Thus, mass specific heat – this is the heat capacity of a unit mass of a substance (1 kg). |
| URI: | http://er.nau.edu.ua/handle/NAU/37947 |
| Appears in Collections: | Aircraft engines |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| A_III_10.pdf | Chapter 10. Heat capacities | 190.2 kB | Adobe PDF | View/Open |
| References.pdf | References | 255.57 kB | Adobe PDF | View/Open |
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