Aircraft engines. Lecture notes (first preliminary edition). Chapter 10. Heat capacities
Репозитарій Національного Авіаційного Університету
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Title |
Aircraft engines. Lecture notes (first preliminary edition). Chapter 10. Heat capacities
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Creator |
Goncharenko, Andriy Viktorovich
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Subject |
aircraft
engine piston type engine gas turbine engine thermodynamic cycle thermodynamic process |
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Description |
Thus, mass specific heat – this is the heat capacity of a unit mass of a substance (1 kg).
The amount of heat which is necessary to be taken in into a body or withdrawn from it in order to change its temperature in 1 °C is called heat capacity [113, pp. 32-36] [79, p. 357]. Heat capacity is calculated by the formula [113, p. 33, (2.37)] |
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Date |
2019-03-01T17:06:26Z
2019-03-01T17:06:26Z 2019-03-01 |
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Type |
Preprint
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Identifier |
http://er.nau.edu.ua/handle/NAU/37947
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Language |
en_US
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Format |
application/pdf
application/pdf |
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Publisher |
National Aviation University
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