Engineering, 23.08.2019 05:10, kharmaculpepper

Consider the twin-jet airplane described in prob. 6.3. the thrust-specific fuel consumption is 1.0 n of fuel per newton of thrust per hour, the fuel capacity is 1900 gal, and the maximum gross weight is 136,960 n. calculate the range and endurance at a standard altitude of 8 km.

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Consider the twin-jet airplane described in prob. 6.3. the thrust-specific fuel consumption is 1.0 n...