he rise of temperature due to the complete combustion of the AERONAUTICAL ENGINES. 119 mixture, say t, may be assumed to be independent of the com-pression ratio. The state of the mixture at C (see diagram) is then represented by a volume —, a temperature (V^-^i), and a pressure Pr /•T-l-f-- After… … Volume of Stroke Fig. 54. initial temperature and pressure. Such an ideal cycle does notconsider {a) the thermal losses due to conduction and radiationthrough the cyhnder walls, and (6) the changes, with tempera-ture, of the properties of the working substance. The efficiency of thiscycle ===—--—,…
Airplanes
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