skip to content

 
Slat Flap
Configuration ds gs/c hs/c df gf/c of/c Description
40 30 0.015 0.015 25 0.010 0.005 part-span flaps, landing configuration
 
 
Nominal Reynold Number (millions)
Data Type
3.5M
6M
9M
12M
15M
Force
uncorrected & corrected
N/A
uncorrected & corrected
uncorrected & corrected
uncorrected & corrected
Pressures - Uncorrected
wing
body
wall/rail/image plane
N/A
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
N/A
wing
body
wing
body
wing
body
Transition
Xtr
N/A
Xtr
Xtr
Xtr
Minituft
images 
N/A
images 
images 
images