TRANSONIC AIRFOIL SECTION C AIRFOIL
    23.       23.

    0.000000  0.000000
    0.001900  0.005700
    0.006000  0.010500
    0.007800  0.012000
    0.012900  0.015700
    0.023700  0.021800
    0.050500  0.032400
    0.079400  0.040200
    0.097500  0.044100
    0.151100  0.052400
    0.203600  0.057600
    0.250000  0.060600
    0.296400  0.062300
    0.346800  0.062900
    0.399000  0.062500
    0.444700  0.060800
    0.490400  0.059700
    0.548600  0.052900
    0.609100  0.047000
    0.657100  0.042200
    0.874100  0.018300
    0.947000  0.007600
    1.000000  0.000000

    0.000000  0.000000
    0.002200 -0.004000
    0.004900 -0.005700
    0.007000 -0.006600
    0.012500 -0.007600
    0.020900 -0.010100
    0.055500 -0.014700
    0.081600 -0.017400
    0.107800 -0.020100
    0.157100 -0.024700
    0.203600 -0.028600
    0.250000 -0.031900
    0.296400 -0.034700
    0.354900 -0.037000
    0.399600 -0.037500
    0.453200 -0.036600
    0.491100 -0.035200
    0.543400 -0.032800
    0.626900 -0.028200
    0.739600 -0.022000
    0.783200 -0.019000
    0.935400 -0.005600
    1.000000 0.000000