Consider our executive jet, weighing W = 9508 N Wing area Sw=3,6 m, Thrust is T=11322...

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Consider our executive jet, weighing W = 9508 N Wing area Sw=3,6 m, Thrust is T=11322 N The polar is CD = 0,016 + 0,05CL². Air density 1,2 kg/m3 Find the max rate of climb in m/sec Round your answer to one decimal digit #.# Consider our executive jet, weighing W = 9508 N Wing area Sw=3,6 m, Thrust is T=11322 N The polar is CD = 0,016 + 0,05CL². Air density 1,2 kg/m3 Find the max rate of climb in m/sec Round your answer to one decimal digit #.#