The Dornier is a light freighter and feeder liner aircraft powered by two Lycoming IGSO-540-A1A six-cylinder horizontally opposed engines, each rated at 260 kW. Assume that Otto cycle represent the...

The Dornier is a light freighter and feeder liner aircraft powered by two Lycoming IGSO-540-A1A six-cylinder horizontally opposed engines, each rated at 260 kW. Assume that Otto cycle represent the cycle for such a spark-ignition engine. Data for the engine is as follows: 1. Compression ratio: 8 2. Temperature and pressure at the beginning of the compression stroke: 300 K and 96 kPa 3. Rate of heat transfer during the constant volume stroke: 760 kJ/kg 4. Specific heat at constant volume: 0.72 kJ/ (kg·K) Shaft Engines 549 Calculate a. The pressure and temperature at the end of the heat addition process b. Network output c. Air mass flow rate d. Mean effective pressure

May 24, 2022
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