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PERCENT OF CHORD (X/C)

CHORD l

OT 'v O
I V
PERCENT O n

<
CLARK - Y BASIC THICKNESS FORM

X/C Y/C % of Chord
$ of Chord Upper Lower
0 3.30 3.30
i 4 1.93
2 4- 6.30 l.h7
...... 2.. . _ . 7.90 0.93
7X 8.83 0.63
.<2 „
10 9.60 O.h2
15 10.69 0.13
20 11.36 0.03
1. 30 11.70 0.00
ho 11. ho 0.00
30 10.32 0.00
60 9.13 0.00
70 7.33 0.00
80_ 3.22 0.00
___ 90 H 2.80 0.00
93 l.h9 0.00
100 0.12 0.00
RAD. L.E. 1.30
INCHES T.E. 0.06“

■ DIMENSIONAL DATA FOR RECOMMENDED
REAR DECK AIRFOIL

FIGURE 2

10