Slat			Flap
Configuration	ds	gs/c	hs/c	df	gf/c	of/c	Description
09	30	0.015	0.015	25	0.015	0.005	part-span flaps, landing configuration

 

	Nominal Reynold Number (millions)
Data Type	3.5M	6M	9M	12M	15M
Force	uncorrected & corrected	uncorrected & corrected	uncorrected & corrected	uncorrected & corrected	uncorrected & corrected
Pressures - Uncorrected	wing body wall/rail/image plane	wing body wall/rail/image plane	wing body wall/rail/image plane	wing body wall/rail/image plane	wing body wall/rail/image plane
Pressures - Corrected to Free Air	wing body	wing body	wing body	wing body	wing body
Transition	Xtr	N/A	Xtr	Xtr	Xtr
Minituft	images	N/A	images	images	images

  Mean Values and Confidence Intervals for Configuration 9  

		3.5M	5.9M	8.8M	11.6M	15M
CL|a=16	avg	1.8813	1.8952	1.8991	1.8994	1.9031
	95% confidence	±0.005	±0.0026	±0.0019	±0.0034	±0.0008
CLmax	avg	2.837	2.9074	2.9315	2.8902	2.9298
	95% confidence	±0.0072	±0.0033	±0.0043	±0.0037	±0.0043
a@CLmax	avg	32.75	34.75	34.88	33.00	34.88
	95% confidence	±0.29	±0.50	±0.48	±0.	±0.25
CLmax-CLmax|Re=3.5M	avg	0.	0.0704	0.0945	0.0532	0.0928
	95% confidence	±	±	±	±	±