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Thread: Static longitudinal stability - converting airspeed to lift coefficient
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Old 27th June 2018 | 11:30
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Gadget freak
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Joined: Apr 2004
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From: England
Originally Posted by Genghis the Engineer
There is no direct readout of climb / descent angle in any aircraft.


G
The velocity vector or flight path marker symbology in many aircraft shows climb/descent angle.
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