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#1
airfoil
#2
trailing edge
#3
wing
#4
plane perpendicular to wing
#5
leading edge
#1
chord
#2
location of maximum camber
#3
location of maximum location
#4
maximum camber
#5
chord line
#6
trailing edge
#7
mean camber line
#8
maximum thickness
#9
leading edge
#1
wing area
#2
root chord
#3
sweep angle
#4
25% chord line
#5
wing kink
#6
span
#7
tip chord