TRANSONIC AIRFOIL SECTION A AIRFOIL
    23.       23.

    0.000000  0.017700
    0.002300  0.030900
    0.005000  0.037200
    0.007600  0.041500
    0.014300  0.049900
    0.024900  0.058200
    0.049500  0.073000
    0.074000  0.081400
    0.099000  0.086600
    0.153000  0.090700
    0.196100  0.090500
    0.250400  0.088700
    0.309400  0.085800
    0.352000  0.083300
    0.391900  0.080400
    0.447700  0.075600
    0.503400  0.069600
    0.559300  0.062600
    0.596500  0.057500
    0.648800  0.049800
    0.835100  0.022400
    0.910900  0.013200
    1.000000  0.000000

    0.000000  0.017700
    0.002200  0.003800
    0.004900 -0.001800
    0.007200 -0.005300
    0.011900 -0.010600
    0.024300 -0.020400
    0.048600 -0.034200
    0.071600 -0.045700
    0.097900 -0.051600
    0.148800 -0.060700
    0.195300 -0.063200
    0.250100 -0.063200
    0.294500 -0.062600
    0.357900 -0.061000
    0.396500 -0.059500
    0.454300 -0.056300
    0.505000 -0.052700
    0.555600 -0.048200
    0.606300 -0.042700
    0.648500 -0.037500
    0.831700 -0.014900
    0.941000 -0.005300
    1.000000 0.000000