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LoadTarget ( FileName ) |
Design Card |
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| Arguments | FileName | the fully qualified name of the file to read, enclosed in double quotes |
| Description | Reads a target pressure distribution from the specified file and initializes the design using th current airfoil shape and the angle of attack and the target Cp distribution read from the file. | |
| Remarks | The input file must contain the pressure coefficient at each coordinate point of airfoil and the design angle of attack in the same format as written by the SaveTarget() command. | |