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DC Field | Value | Language |
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dc.contributor.author | Goncharenko, Andriy Viktorovich | en |
dc.date.accessioned | 2019-03-01T17:06:26Z | - |
dc.date.available | 2019-03-01T17:06:26Z | - |
dc.date.issued | 2019-03-01 | - |
dc.identifier.uri | http://er.nau.edu.ua/handle/NAU/37947 | - |
dc.description | Thus, mass specific heat – this is the heat capacity of a unit mass of a substance (1 kg). | en |
dc.description.abstract | The amount of heat which is necessary to be taken in into a body or withdrawn from it in order to change its temperature in 1 °C is called heat capacity.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. | en |
dc.language.iso | en | en |
dc.publisher | National Aviation University | en |
dc.subject | aircraft | en |
dc.subject | engine | en |
dc.subject | piston type engine | en |
dc.subject | gas turbine engine | en |
dc.subject | thermodynamic cycle | en |
dc.subject | thermodynamic process | en |
dc.title | Aircraft engines. Lecture notes (first preliminary edition). Chapter 10. Heat capacities | en |
dc.type | Preprint | en |
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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