Aircraft engines. Lecture notes (first preliminary edition). Chapter 10. Heat capacities
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Date
2019-03-01
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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The amount of heat which is necessary to be taken in into a body or withdrawn from it in order to change its temperature in 1 °C is called heat capacity.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).
Keywords
aircraft, engine, piston type engine, gas turbine engine, thermodynamic cycle, thermodynamic process