Related articles:
Airfoil
Key terms:
y
math
chord
naca
airfoil
digit
frac
left
right
camber
describing
give
surface
pressure
upper
theta
lower
example
design
leading edge
maximum thickness
shape
formula
lift coefficient
begin
located
generator
hyphen
maximum camber
profile
chord back
laminar flow
series airfoil
coordinates
naca airfoil
tens of percent of chord
airfoil surface
above and below
minimum pressure area
one digit describing the distance
distance of maximum
lift coefficient in tenths
fraction of the chord
indicating the series
distance of the minimum pressure
digits in the following sequence
two digits describing the maximum
digits describing the maximum thickness
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