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


the latest version is available at
https://github.com/John-Bray/C101



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