## What airfoil section data formats are supported by Code Wand?

The following airfoil section data formats are supported by Code Wand.

## Supported Input Format |
## Comments |
---|---|

(x,rθ,r) | Defined trailing edge to trailing edge |

(x_{1},y_{1},z_{1},x_{2},y_{2},z_{2}) |
Defined leading edge to trailing edge |

CFX format (x,y,z) | Defined leading edge to leading edge |

Suction(x,y,z) & Pressure(x,y,z) | Defined leading edge to trailing edge |

(x_{1},y_{1},y_{2}) |
Defined leading edge to trailing edge at a given spanwise location |

(x,y) at constant radius | Defined trailing edge to trailing edge at a given spanwise location |

(x_{1},rθ_{1},x_{2},rθ_{2}) |
Defined leading edge to trailing edge at a given spanwise location |

(x_{1},rθ_{1},x_{2},rθ_{2},r_{1},r_{2}) |
Defined leading edge to trailing edge |

(x_{1},t_{1},r_{1},x_{2},t_{2},r_{2}) |
Defined leading edge to trailing edge |

(-y_{1},x_{1},-y_{2},x_{2}) |
Defined leading edge to trailing edge at a given spanwise location |

(x_{1},rθ_{1} all) |
Read spanwise location, then all x_{1} values then all rθ_{1} values |

**Code**

**Author**

George Fan

**Date Created**

2013-06-11 02:46:45

**Date Updated**

2013-06-11 02:46:45

**Views**

4338