Data for standard temperature and pressure
In the course of testing my -6A project, I have gathered stall speeds, approximate takeoff and landing distances, and will be gathering a number of data points around climb performance. However, none of these flights have taken place at standard temperature (15 ?C / 59 ?F) or pressure (29.92).
Is there an established method for translating data at nonstandard temps/pressures to standard? My goal is to produce a set of performance charts for my POH similar to what you might find in the POH for a factory aircraft.
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Brad Benson, Maplewood MN.
RV-6A N164BL, Flying since Nov 2012!
If you're not making mistakes, you're probably not making anything
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