C101 Landing test
Testing the adjusted attitude / CofG changes landing at LEAM (Almeria)
Here is a version with test equipment to monitor what is happening in more detail (LEGR, Granada)
No flaps stall is just over 14 degrees alpha, 110 knots
Full flaps stall is about 13.5 degrees alpha, 100 knots
For comparison, the stock Cessna manages around 8 degrees alpha on landing
The stock 737 manages around 10 degrees alpha on landing
https://github.com/John-Bray/C101
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