Table 2.

Influence of elevator deflection on lift force coefficient.

dH°	−30°	−20°	−10°	0°	10°	20°	30°
α° (CL = 0)	2	1.5	1	1	0.5	0	0.5
CL (α = −10°)	−0.89919	−0.8909	−0.85761	−0.7930	−0.75293	−0.73197	−0.68523
CL (α = 0°)	−0.1699	−0.1425	−0.1178	−0.079	−0.0394	−0.0047	0.02893
CL (α = 10°)	0.57024	0.6099	0.63362	0.68967	0.72973	0.75795	0.79622
CL min	−0.9675	−0.9937	−0.9402	−0.9100	−0.8646	−0.8349	−0.8252
αcr°	12	12	12	12	12	12	12
CL max	0.8030	0.8101	0.8405	0.8611	0.8734	0.8912	0.90296