input_c14.json

{
    "C14" : {
        "airfoil dat file location" : "NACA 0009.txt",
        "chord [in]" : 12.0,
        "num arcs" : 5,
        "num arc points" : 30,
        "arc concave" : true,
        "arc type" : "exponential",
        "arc type notes" : "'exponential','reversed_exp', '90%t', or 'hinge_point'",
        "section resolution" : 400,
        "shell thickness [mm]" : 0.8,
        "flex start [x/c]" : 0.5,
        "tongue start [in]" : 1.0,
        "tongue start [in]_notes" : "distance before flex start",
        "mouth start [in]" : 2.0,
        "mouth start [in]_notes" : "distance before flex start",
        "TE wall start [x/c]" : 0.95,
        "mouth clearance [mm]" :  1.0,
        "fillet side length [mm]" : 1.0,
        "enthicken" : 1.0,
        "Notes" : " ",
        "skip wing box" : true,
        "show plot" : true,
        "write dxf" : false,
        "shift to c/4" : false,
        "split return" : false,
        "guide curve return" : false,
        "actuation hole return" : false,
        "show legend" : false,
        "all black" : true,
        "deflection angle [deg]" : [-15.0],
        "deflection type" : "parabolic",
        "deflection type notes" : "'none', 'traditional', or 'parabolic'",
        "hinge at top" : true,
        "dxf file path" : "/home/ben/Desktop/",
        "dxf file name" : "c14"
    }
}