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Lower lift curve slope than in real life, more induced drag


mytai01

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1 hour ago, oldtimesake said:

Did you see that?

 

A DCS clean F-16C-50 needs 23.3deg AOA to reach 8.5G at mach 0.75, while a loaded real life F-16C-50 needs only 15deg AOA to reach 9G at mach 0.67!

 

WTF is that lift curve slope, ED? 

 

It's WIP. They're revisiting the FM soon. It won't be left like this. EA is a long process.

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