European Transport Research Review

An Open Access Journal

Table 4 Flight behaviour

From: A new aircraft architecture based on the ACHEON Coanda effect nozzle: flight model and energy evaluation

	Angle of Attack	Angle of Climb	Pitch Attitude	Incidence	Airspeed
Initial roll	4.5^∘	0^∘	0.0^∘	4.5^∘	Small, incr.
After rotation	12.0^∘	0^∘	7.5^∘	4.5^∘	increasing
At liftoff	12.0^∘	0^∘	7.5^∘	4.5^∘	6 % below V _Y
Initial climb	Decr.	incr.	7.5^∘	4.5^∘	increasing
Steady climb	7.0^∘	5^∘	7.5^∘	4.5^∘	10 % above V

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