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I wonder if its possible to convert the figures to different altitudes..?
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Is the question asked and I answered.
http://forum.1cpublishing.eu/showpos...&postcount=166
My post was not a treatsie on specific aircraft performance.
It took a few seconds to say, "Yes you can use EAS to convert the performance to any altitude" with any airplane.
And did the correct mathmatical mechanics to show the process to change altitudes given a speed and angle of bank.
As for the other baloney posted,
it will always reach CLmax at the lift line irregardless of altitude in the theory the RAE is using.
That should not be a surprise to a MSc Aerospace Engineering.
Any undergraduate who has taken a Basic Aerodynamics course understands that. It is a principle of subsonic incompressible flow theory.