#59 The Dornier is a light freighter and feeder liner aircraft powered
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#59 The Dornier is a light freighter and feeder liner aircraft powered
#59 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 the Otto cycle represent the cycle for such a spark-ignition engine. Data for the engine is as follows
Compression ratio: 8
Temperature and pressure at the beginning of the compression stroke: 300 K and 96 kPa
Rate of heat transfer during the constant volume stroke: 760 kJ/kg.
Specific heat at constant volume: 0.72 kJ/(kg · K)
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
Get the Free Online Chemistry Q&A Questions And Answers with explain. To crack any examinations and Interview tests these Chemistry Questions And Answers are very useful. Here we have uploaded the Free Online Chemistry Questions. Here we are also given the all chemistry topic.
ChemistryExplain team has covered all Topics related to inorganic, organic, physical chemistry, and others So, Prepare these Chemistry Questions and Answers with Explanation Pdf.
Question
#59 The Dornier is a light freighter and feeder liner aircraft powered
#59 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 the Otto cycle represent the cycle for such a spark-ignition engine. Data for the engine is as follows
Compression ratio: 8
Temperature and pressure at the beginning of the compression stroke: 300 K and 96 kPa
Rate of heat transfer during the constant volume stroke: 760 kJ/kg.
Specific heat at constant volume: 0.72 kJ/(kg · K)
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
Answer
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