PPRuNe Forums - View Single Post - A320 IAE V2500 powered VS A320 CFM powered?

21st Jan 2017, 12:20

#31 (permalink)

KayPam

Join Date: Dec 2015

Location: France

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I think it should be a little more, shouldn't it ?
Thrust should not decrease faster than atmospheric pressure, else you're not gonna be faster at altitude.
You're gonna be slower because of greater drag (due to greater Coefficient of Lift required)

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