Calculate the total thrust under the following conditions

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Consider a twin-spool turbofan engine with the fan driven by the LP turbine and the compressor by the HP turbine. Separate cold and hot exhaust nozzles are used. Calculate the total thrust under the following conditions.

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Assume sea level static conditions where the ambient pressure and temperature are 1.0 bar and 300 K, respectively.

Reference no: EM131285135

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